Compare commits
10 Commits
1e6d352e00
...
bd37295da9
| Author | SHA1 | Date | |
|---|---|---|---|
| bd37295da9 | |||
| e83da3156b | |||
| 07ccac9c2a | |||
| 1a97b9e986 | |||
| ee4590276a | |||
| 945784a7cf | |||
| c798cc8547 | |||
| b992a1dd5f | |||
| ad4c3ada92 | |||
| 432e5a737a |
1356
Cargo.lock
generated
1356
Cargo.lock
generated
File diff suppressed because it is too large
Load Diff
13
Cargo.toml
13
Cargo.toml
@ -7,6 +7,19 @@ edition = "2024"
|
|||||||
bevy = "0.16"
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bevy = "0.16"
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||||||
bevy-inspector-egui = "0.33.1"
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bevy-inspector-egui = "0.33.1"
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||||||
bevy_panorbit_camera = "0.26"
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bevy_panorbit_camera = "0.26"
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||||||
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big_space = { version = "0.10.0", features = ["camera"] }
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||||||
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chrono = "0.4.41"
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futures = "0.3.31"
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iyes_perf_ui = "0.5.0"
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||||||
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rayon = "1.11.0"
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||||||
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regex = "1.11.1"
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||||||
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reqwest = { version = "0.12", features = ["json"] }
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rhorizons = "0.5.0"
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ron = "0.10.1"
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||||||
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serde = { version = "1.0", features = ["derive"] }
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||||||
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serde_json = "1.0"
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||||||
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thiserror = "2.0"
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||||||
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tokio = { version = "1.47.1", features = ["full"] }
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||||||
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||||||
# Enable a small amount of optimization in the dev profile.
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# Enable a small amount of optimization in the dev profile.
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||||||
[profile.dev]
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[profile.dev]
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||||||
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|||||||
328
assets/initial_state.ron
Normal file
328
assets/initial_state.ron
Normal file
@ -0,0 +1,328 @@
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|||||||
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// mass kg f64
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||||||
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// radius km f64
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||||||
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// position au f64
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||||||
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// velocity au/day f64
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||||||
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||||||
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(
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||||||
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bodies: [
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||||||
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(
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||||||
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name: "Sun",
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||||||
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mass: 1.98841e30,
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||||||
|
radius: 695700.0,
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||||||
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position: (0.0, 0.0, 0.0),
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||||||
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velocity: (0.0, 0.0, 0.0),
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||||||
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model: (
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||||||
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path: "sun.glb",
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||||||
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scale: (4.016625881e-2, 4.016625881e-2, 4.016625881e-2),
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||||||
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),
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||||||
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),
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||||||
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(
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||||||
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name: "Mercury",
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||||||
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mass: 3.302e23,
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||||||
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radius: 2439.4,
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||||||
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position: (-3.873030085256687e-01, -1.617241946342014e-01, 2.230772540124238e-02),
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||||||
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velocity: (5.024430196457658e-03, -2.474345331076241e-02, -2.482923861184285e-03),
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||||||
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model: (
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||||||
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path: "mercury.glb",
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||||||
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scale: (1.409040560e-4, 1.407730015e-4, 1.409040560e-4),
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||||||
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),
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||||||
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),
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||||||
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(
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||||||
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name: "Venus",
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||||||
|
mass: 4.8685e24,
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||||||
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radius: 6051.84,
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||||||
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position: (4.534187654737982e-01, 5.622160792960551e-01, -1.844136025242647e-02),
|
||||||
|
velocity: (-1.580627428004959e-02, 1.261006264179427e-02, 1.085217883057661e-03),
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||||||
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model: (
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||||||
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path: "venus.glb",
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||||||
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scale: (3.494008561e-4, 3.494008561e-4, 3.494008561e-4),
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||||||
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),
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||||||
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),
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||||||
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(
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||||||
|
name: "Earth",
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||||||
|
mass: 5.97219e24,
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||||||
|
radius: 6371.01,
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||||||
|
position: (-1.786834409731047e-01, 9.669827953774551e-01, -5.109423915082682e-05),
|
||||||
|
velocity: (-1.720473858166942e-02, -3.193533189307208e-03, 5.457174067040888e-09),
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||||||
|
model: (
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||||||
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path: "earth.glb",
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||||||
|
scale: (3.686534474e-4, 3.674174368e-4, 3.686534474e-4),
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||||||
|
),
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||||||
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),
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||||||
|
(
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||||||
|
name: "Mars",
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||||||
|
mass: 6.4171e23,
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||||||
|
radius: 3389.92,
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||||||
|
position: (-5.216858665681381e-01, 1.525234576802456e+00, 4.475559803760917e-02),
|
||||||
|
velocity: (-1.271183490340250e-02, -3.338839586395265e-03, 2.417788175776839e-04),
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||||||
|
model: (
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||||||
|
path: "mars.glb",
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||||||
|
scale: (1.964640105e-4, 1.953076135e-4, 1.964640105e-4),
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||||||
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),
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||||||
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),
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||||||
|
(
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||||||
|
name: "Jupiter",
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||||||
|
mass: 1.89819e27,
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||||||
|
radius: 69911.0,
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||||||
|
position: (1.056033545576702e+00, 4.971452162023883e+00, -4.427806378454757e-02),
|
||||||
|
velocity: (-7.476272400979211e-03, 1.924466075080766e-03, 1.592575331437652e-04),
|
||||||
|
model: (
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||||||
|
path: "jupiter.glb",
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||||||
|
scale: (4.216764122e-3, 3.943203948e-3, 4.216764122e-3),
|
||||||
|
),
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||||||
|
),
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||||||
|
(
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||||||
|
name: "Saturn",
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||||||
|
mass: 5.6834e26,
|
||||||
|
radius: 58232.0,
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||||||
|
position: (9.461067271500818e+00, -1.764614720843175e+00, -3.458764004169705e-01),
|
||||||
|
velocity: (7.093807804551229e-04, 5.475097536527790e-03, -1.232345969963958e-04),
|
||||||
|
model: (
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||||||
|
path: "saturn.glb",
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||||||
|
scale: (1.828302280e-3, 1.649197191e-3, 1.828302280e-3),
|
||||||
|
),
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||||||
|
),
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||||||
|
(
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||||||
|
name: "Uranus",
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||||||
|
mass: 8.6813e25,
|
||||||
|
radius: 25362.0,
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||||||
|
position: (1.110362881512566e+01, 1.609448391218202e+01, -8.419833258524990e-02),
|
||||||
|
velocity: (-3.273728238819980e-03, 2.053528328895527e-03, 5.008589052969062e-05),
|
||||||
|
model: (
|
||||||
|
path: "uranus.glb",
|
||||||
|
scale: (1.486925757e-3, 1.452834462e-3, 1.486925757e-3),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Neptune",
|
||||||
|
mass: 1.02409e26,
|
||||||
|
radius: 24624.0,
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||||||
|
position: (2.987992735576156e+01, -6.341879950443392e-01, -6.754997950415415e-01),
|
||||||
|
velocity: (3.941595250081164e-05, 3.160389775728832e-03, -6.636996572427530e-05),
|
||||||
|
model: (
|
||||||
|
path: "neptune.glb",
|
||||||
|
scale: (1.437890343e-3, 1.413329272e-3, 1.437890343e-3),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Moon",
|
||||||
|
mass: 7.349e22,
|
||||||
|
radius: 1737.53,
|
||||||
|
position: (-1.776670337217189e-01, 9.646511868801392e-01, -2.560710414773878e-04),
|
||||||
|
velocity: (-1.666610342674751e-02, -2.935662211368250e-03, 2.214641479437884e-05),
|
||||||
|
model: (
|
||||||
|
path: "moon.glb",
|
||||||
|
scale: (1.003505604e-4, 1.003505604e-4, 1.003505604e-4),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Phobos",
|
||||||
|
mass: 1.08e16,
|
||||||
|
radius: 11.1,
|
||||||
|
position: (-5.216607506283159e-01, 1.525290094552813e+00, 4.474552444674667e-02),
|
||||||
|
velocity: (-1.371531677510715e-02, -2.797359927923991e-03, 7.604209362929195e-04),
|
||||||
|
model: (
|
||||||
|
path: "phobos.glb",
|
||||||
|
scale: (3.111071419e-5, 2.177749957e-5, 2.728170512e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Deimos",
|
||||||
|
mass: 1.80e15,
|
||||||
|
radius: 6.2,
|
||||||
|
position: (-5.215476623931578e-01, 1.525280501692070e+00, 4.469744727198185e-02),
|
||||||
|
velocity: (-1.290124900899404e-02, -2.594527535740538e-03, 3.799855876623048e-04),
|
||||||
|
model: (
|
||||||
|
path: "deimos.glb",
|
||||||
|
scale: (3.572769492e-5, 2.336041507e-5, 2.748284533e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Io",
|
||||||
|
mass: 8.93e22,
|
||||||
|
radius: 1821.49,
|
||||||
|
position: (1.053815818667817e+00, 4.969715993299296e+00, -4.437108516416628e-02),
|
||||||
|
velocity: (-1.329530996368361e-03, -5.983335980023409e-03, -3.295420474951598e-05),
|
||||||
|
model: (
|
||||||
|
path: "io.glb",
|
||||||
|
scale: (1.056204637e-4, 1.048294944e-4, 1.050431092e-4),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Europa",
|
||||||
|
mass: 4.80e22,
|
||||||
|
radius: 1560.8,
|
||||||
|
position: (1.060479105966296e+00, 4.971193788432235e+00, -4.418907806556983e-02),
|
||||||
|
velocity: (-6.967074192246404e-03, 9.896683771810605e-03, 4.296001484155991e-04),
|
||||||
|
model: (
|
||||||
|
path: "europa.glb",
|
||||||
|
scale: (9.021675214e-5, 9.003777086e-5, 9.008396592e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Ganymede",
|
||||||
|
mass: 1.48e23,
|
||||||
|
radius: 2631.2,
|
||||||
|
position: (1.062520398626604e+00, 4.968458682597362e+00, -4.429967587277176e-02),
|
||||||
|
velocity: (-4.841408463186764e-03, 7.634290231598638e-03, 4.147177169244575e-04),
|
||||||
|
model: (
|
||||||
|
path: "ganymede.glb",
|
||||||
|
scale: (1.519124053e-4, 1.519124053e-4, 1.519124053e-4),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Callisto",
|
||||||
|
mass: 1.08e23,
|
||||||
|
radius: 2410.3,
|
||||||
|
position: (1.046927187861326e+00, 4.980213520221207e+00, -4.412635447845523e-02),
|
||||||
|
velocity: (-1.076662893789138e-02, -1.453153071657253e-03, 9.400054299331563e-06),
|
||||||
|
model: (
|
||||||
|
path: "callisto.glb",
|
||||||
|
scale: (1.391587430e-4, 1.391587430e-4, 1.391587430e-4),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Mimas",
|
||||||
|
mass: 3.75e19,
|
||||||
|
radius: 198.8,
|
||||||
|
position: (9.462113317387443e+00, -1.764120396234732e+00, -3.462575454806998e-01),
|
||||||
|
velocity: (-3.600569225193193e-03, 1.195945377622506e-02, -3.321658418910402e-03),
|
||||||
|
model: (
|
||||||
|
path: "mimas.glb",
|
||||||
|
scale: (3.022084638e-5, 2.771941035e-5, 2.860654604e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Enceladus",
|
||||||
|
mass: 1.0805e20,
|
||||||
|
radius: 252.3,
|
||||||
|
position: (9.462107070733344e+00, -1.763590731315564e+00, -3.465134777458668e-01),
|
||||||
|
velocity: (-4.799068161710644e-03, 9.904458072213898e-03, -1.910803547584920e-03),
|
||||||
|
model: (
|
||||||
|
path: "enceladus.glb",
|
||||||
|
scale: (1.481480831e-5, 1.433560737e-5, 1.451458593e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Tethys",
|
||||||
|
mass: 6.176e20,
|
||||||
|
radius: 536.3,
|
||||||
|
position: (9.463028141754283e+00, -1.764725184828637e+00, -3.460263238634043e-01),
|
||||||
|
velocity: (8.124741088132637e-04, 1.132977234261396e-02, -3.072248079372077e-03),
|
||||||
|
model: (
|
||||||
|
path: "tethys.glb",
|
||||||
|
scale: (3.129428660e-5, 3.059098162e-5, 3.070722960e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Dione",
|
||||||
|
mass: 1.09572e21,
|
||||||
|
radius: 562.5,
|
||||||
|
position: (9.460669031566509e+00, -1.762393870120674e+00, -3.470001695782450e-01),
|
||||||
|
velocity: (-4.995042476514132e-03, 4.898468069198046e-03, 7.315317142172153e-04),
|
||||||
|
model: (
|
||||||
|
path: "dione.glb",
|
||||||
|
scale: (3.252791430e-5, 3.230852235e-5, 3.240667138e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Rhea",
|
||||||
|
mass: 2.309e21,
|
||||||
|
radius: 764.5,
|
||||||
|
position: (9.463441058546145e+00, -1.766997606737125e+00, -3.448366300385151e-01),
|
||||||
|
velocity: (4.307393238751094e-03, 8.273257376182423e-03, -1.932435874857194e-03),
|
||||||
|
model: (
|
||||||
|
path: "rhea.glb",
|
||||||
|
scale: (4.416729644e-5, 4.401718616e-5, 4.405760046e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Titan",
|
||||||
|
mass: 1.34553e23,
|
||||||
|
radius: 2575.5,
|
||||||
|
position: (9.468440328490537e+00, -1.762284834421733e+00, -3.478122131916790e-01),
|
||||||
|
velocity: (-4.611400435334967e-04, 8.260265884102586e-03, -1.443082816825538e-03),
|
||||||
|
model: (
|
||||||
|
path: "titan.glb",
|
||||||
|
scale: (1.486763649e-4, 1.486371038e-4, 1.486549882e-4),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Iapetus",
|
||||||
|
mass: 1.8059e21,
|
||||||
|
radius: 734.5,
|
||||||
|
position: (9.454548058738080e+00, -1.786906158368561e+00, -3.394196336672040e-01),
|
||||||
|
velocity: (2.477125925502744e-03, 4.942920731685813e-03, -3.564738618756286e-04),
|
||||||
|
model: (
|
||||||
|
path: "iapetus.glb",
|
||||||
|
scale: (4.305300899e-5, 4.111311500e-5, 4.305300899e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Miranda",
|
||||||
|
mass: 6.59e19,
|
||||||
|
radius: 235.8,
|
||||||
|
position: (1.110338075481133e+01, 1.609470886437212e+01, -8.339848717695617e-02),
|
||||||
|
velocity: (2.787135511093017e-04, 1.302160355796409e-03, 1.366210183434322e-03),
|
||||||
|
model: (
|
||||||
|
path: "miranda.glb",
|
||||||
|
scale: (1.387950124e-5, 1.344648808e-5, 1.352154413e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Ariel",
|
||||||
|
mass: 1.25e21,
|
||||||
|
radius: 578.9,
|
||||||
|
position: (1.110453239435098e+01, 1.609416926126415e+01, -8.504238243640228e-02),
|
||||||
|
velocity: (-5.417334967749265e-03, 2.196892645955784e-03, -2.298152372242362e-03),
|
||||||
|
model: (
|
||||||
|
path: "ariel.glb",
|
||||||
|
scale: (3.354982618e-5, 3.335352449e-5, 3.336507143e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Umbriel",
|
||||||
|
mass: 1.28e21,
|
||||||
|
radius: 584.7,
|
||||||
|
position: (1.110253678329407e+01, 1.609490555702174e+01, -8.286998450094619e-02),
|
||||||
|
velocity: (-1.219602563560983e-03, 1.849034126664038e-03, 1.801100761916168e-03),
|
||||||
|
model: (
|
||||||
|
path: "umbriel.glb",
|
||||||
|
scale: (3.375767119e-5, 3.375767119e-5, 3.375767119e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Titania",
|
||||||
|
mass: 3.34e21,
|
||||||
|
radius: 788.9,
|
||||||
|
position: (1.110510884778205e+01, 1.609382177197045e+01, -8.661833178512783e-02),
|
||||||
|
velocity: (-5.032495225759578e-03, 2.280002002691279e-03, -1.088327315015861e-03),
|
||||||
|
model: (
|
||||||
|
path: "titania.glb",
|
||||||
|
scale: (4.554716361e-5, 4.554716361e-5, 4.554716361e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Oberon",
|
||||||
|
mass: 3.08e21,
|
||||||
|
radius: 761.4,
|
||||||
|
position: (1.110301190463219e+01, 1.609515778477002e+01, -8.040210462613612e-02),
|
||||||
|
velocity: (-1.519780917379062e-03, 1.720169702110850e-03, 3.926675849694972e-04),
|
||||||
|
model: (
|
||||||
|
path: "oberon.glb",
|
||||||
|
scale: (4.395945143e-5, 4.395945143e-5, 4.395945143e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
(
|
||||||
|
name: "Triton",
|
||||||
|
mass: 2.14e22,
|
||||||
|
radius: 1352.6,
|
||||||
|
position: (2.987802053077272e+01, -6.355569689698364e-01, -6.751627943073906e-01),
|
||||||
|
velocity: (-6.787804924900204e-04, 4.636375429506899e-03, 1.865945736548040e-03),
|
||||||
|
model: (
|
||||||
|
path: "triton.glb",
|
||||||
|
scale: (7.809240196e-5, 7.809240196e-5, 7.809240196e-5),
|
||||||
|
),
|
||||||
|
),
|
||||||
|
],
|
||||||
|
)
|
||||||
115
assets/jpl_horizon/bodies/Ariel.txt
Normal file
115
assets/jpl_horizon/bodies/Ariel.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 29, 2025 Ariel / (Uranus) 701
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 581.1x577.9x577.7 Density (g cm^-3) = 1.54 +- 0.026
|
||||||
|
GM (km^3/s^2) = 83.43 +- 1.40 Geometric Albedo = 0.34
|
||||||
|
V(1,0) = +1.45
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to equatorial plane & IAU pole)
|
||||||
|
Semi-major axis, a (km) = 191.2 (10^3) Orbital period = 2.520 d
|
||||||
|
Eccentricity, e = 0.0034 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 179.69
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:46 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Ariel (701) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110453239435098E+01 Y = 1.609416926126415E+01 Z =-8.504238243640228E-02
|
||||||
|
VX=-5.417334967749265E-03 VY= 2.196892645955784E-03 VZ=-2.298152372242362E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110452863095813E+01 Y = 1.609417078735579E+01 Z =-8.504397710872791E-02
|
||||||
|
VX=-5.421235378195795E-03 VY= 2.198251211682732E-03 VZ=-2.294502747948997E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
114
assets/jpl_horizon/bodies/Callisto.txt
Normal file
114
assets/jpl_horizon/bodies/Callisto.txt
Normal file
@ -0,0 +1,114 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Mar 12, 2021 Callisto / (Jupiter) 504
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean radius (km) = 2410.3 +- 1.5 Density (g cm^-3)= 1.834 +- 0.004
|
||||||
|
GM (km^3/s^2) = 7179.2834 +- 0.0097 Geometric Albedo = 0.17 +- 0.02
|
||||||
|
|
||||||
|
SATELLITE ORBIT (at J2000.0 epoch, 2000-Jan-1.5):
|
||||||
|
Semi-major axis, a (km)~ 1,883,000 Orbital period ~ 16.691 d
|
||||||
|
Eccentricity, e ~ 0.00744 Rotational period= Synchronous
|
||||||
|
Inclination, i (deg) ~ 0.200
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:34 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Callisto (504) {source: jup365_merged}
|
||||||
|
Center body name: Sun (10) {source: jup365_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.046927187861326E+00 Y = 4.980213520221207E+00 Z =-4.412635447845523E-02
|
||||||
|
VX=-1.076662893789138E-02 VY=-1.453153071657253E-03 VZ= 9.400054299331563E-06
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.046919711342476E+00 Y = 4.980212510788754E+00 Z =-4.412634795573506E-02
|
||||||
|
VX=-1.076574531183088E-02 VY=-1.454012353275114E-03 VZ= 9.385381807833990E-06
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Deimos.txt
Normal file
115
assets/jpl_horizon/bodies/Deimos.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jun 02, 2025 Deimos / (Mars) 402
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 7.8 x 6.0 x 5.1 Density (g cm^-3) = 1.76 +- 0.30
|
||||||
|
Mass (10^20 kg ) = 1.80 (10^-5) Geometric Albedo = 0.06
|
||||||
|
(+- 0.15) V(1,0) = +12.89
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA:
|
||||||
|
Semi-major axis, a (km) = 23.4632(10^3) Orbital period = 1.263 d
|
||||||
|
Eccentricity, e = 0.00033 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 1.791
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:28 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Deimos (402) {source: mar099}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X =-5.215476623931578E-01 Y = 1.525280501692070E+00 Z = 4.469744727198185E-02
|
||||||
|
VX=-1.290124900899404E-02 VY=-2.594527535740538E-03 VZ= 3.799855876623048E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X =-5.215566224100128E-01 Y = 1.525278699635617E+00 Z = 4.469771149715475E-02
|
||||||
|
VX=-1.290359915493358E-02 VY=-2.595396531058469E-03 VZ= 3.809826346570343E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Dione.txt
Normal file
117
assets/jpl_horizon/bodies/Dione.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Dione / (Saturn) 604
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 562.5 +- 5 Density (g/cm^3) = 1.469 +- 0.012
|
||||||
|
Mass (10^19 kg) = 109.572 Geometric Albedo = 0.6
|
||||||
|
GM (km^3/s^2) = 73.116 +- 0.02 V(1,0) = +0.8
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean values referred to local Laplace plane):
|
||||||
|
Semi-major axis, a (km) = 377.42(10^3) Orbital period = 2.736915 d
|
||||||
|
Eccentricity, e = 0.0022 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 0.028
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:39 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Dione (604) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.460669031566509E+00 Y =-1.762393870120674E+00 Z =-3.470001695782450E-01
|
||||||
|
VX=-4.995042476514132E-03 VY= 4.898468069198046E-03 VZ= 7.315317142172153E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.460665563295446E+00 Y =-1.762390471236195E+00 Z =-3.469996601384587E-01
|
||||||
|
VX=-4.993575760054306E-03 VY= 4.890319489938703E-03 VZ= 7.356544990270154E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
@ -1,152 +1,131 @@
|
|||||||
curl -s "https://ssd.jpl.nasa.gov/api/horizons.api?format=text&COMMAND=%27399%27&CENTER=%27%40sun%27&EPHEM_TYPE=%27VECTORS%27&OUT_UNITS=%27AU-D%27&START_TIME=%272000-01-01%2012:00%27&STOP_TIME=%272000-01-01%2012:01%27&STEP_SIZE=%271%20m%27&VEC_TABLE=2&REF_PLANE=%27ECLIPTIC%27&REF_SYSTEM=%27J2000%27"
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
API VERSION: 1.2
|
|
||||||
API SOURCE: NASA/JPL Horizons API
|
*******************************************************************************
|
||||||
|
Revised: April 12, 2021 Earth 399
|
||||||
*******************************************************************************
|
|
||||||
Revised: April 12,
|
GEOPHYSICAL PROPERTIES (revised May 9, 2022):
|
||||||
2021 Earth 399
|
Vol. Mean Radius (km) = 6371.01+-0.02 Mass x10^24 (kg)= 5.97219+-0.0006
|
||||||
|
Equ. radius, km = 6378.137 Mass layers:
|
||||||
GEOPHYSICAL PROPERTIES (revised May 9,
|
Polar axis, km = 6356.752 Atmos = 5.1 x 10^18 kg
|
||||||
2022):
|
Flattening = 1/298.257223563 oceans = 1.4 x 10^21 kg
|
||||||
Vol. Mean Radius (km) = 6371.01+-0.02 Mass x10^24 (kg)= 5.97219+-0.0006
|
Density, g/cm^3 = 5.51 crust = 2.6 x 10^22 kg
|
||||||
Equ. radius, km = 6378.137 Mass layers:
|
J2 (IERS 2010) = 0.00108262545 mantle = 4.043 x 10^24 kg
|
||||||
Polar axis, km = 6356.752 Atmos = 5.1 x 10^18 kg
|
g_p, m/s^2 (polar) = 9.8321863685 outer core = 1.835 x 10^24 kg
|
||||||
Flattening = 1/298.257223563 oceans = 1.4 x 10^21 kg
|
g_e, m/s^2 (equatorial) = 9.7803267715 inner core = 9.675 x 10^22 kg
|
||||||
Density, g/cm^3 = 5.51 crust = 2.6 x 10^22 kg
|
g_o, m/s^2 = 9.82022 Fluid core rad = 3480 km
|
||||||
J2 (IERS 2010) = 0.00108262545 mantle = 4.043 x 10^24 kg
|
GM, km^3/s^2 = 398600.435436 Inner core rad = 1215 km
|
||||||
g_p, m/s^2 (polar) = 9.8321863685 outer core = 1.835 x 10^24 kg
|
GM 1-sigma, km^3/s^2 = 0.0014 Escape velocity = 11.186 km/s
|
||||||
g_e, m/s^2 (equatorial) = 9.7803267715 inner core = 9.675 x 10^22 kg
|
Rot. Rate (rad/s) = 0.00007292115 Surface area:
|
||||||
g_o, m/s^2 = 9.82022 Fluid core rad = 3480 km
|
Mean sidereal day, hr = 23.9344695944 land = 1.48 x 10^8 km
|
||||||
GM, km^3/s^2 = 398600.435436 Inner core rad = 1215 km
|
Mean solar day 2000.0, s = 86400.002 sea = 3.62 x 10^8 km
|
||||||
GM 1-sigma, km^3/s^2 = 0.0014 Escape velocity = 11.186 km/s
|
Mean solar day 1820.0, s = 86400.0 Love no., k2 = 0.299
|
||||||
Rot. Rate (rad/s) = 0.00007292115 Surface area:
|
Moment of inertia = 0.3308 Atm. pressure = 1.0 bar
|
||||||
Mean sidereal day, hr = 23.9344695944 land = 1.48 x 10^8 km
|
Mean surface temp (Ts), K= 287.6 Volume, km^3 = 1.08321 x 10^12
|
||||||
Mean solar day 2000.0, s = 86400.002 sea = 3.62 x 10^8 km
|
Mean effect. temp (Te), K= 255 Magnetic moment = 0.61 gauss Rp^3
|
||||||
Mean solar day 1820.0, s = 86400.0 Love no., k2 = 0.299
|
Geometric albedo = 0.367 Vis. mag. V(1,0)= -3.86
|
||||||
Moment of inertia = 0.3308 Atm. pressure = 1.0 bar
|
Solar Constant (W/m^2) = 1367.6 (mean), 1414 (perihelion), 1322 (aphelion)
|
||||||
Mean surface temp (Ts), K= 287.6 Volume, km^3 = 1.08321 x 10^12
|
HELIOCENTRIC ORBIT CHARACTERISTICS:
|
||||||
Mean effect. temp (Te), K= 255 Magnetic moment = 0.61 gauss Rp^3
|
Obliquity to orbit, deg = 23.4392911 Sidereal orb period = 1.0000174 y
|
||||||
Geometric albedo = 0.367 Vis. mag. V(1,
|
Orbital speed, km/s = 29.79 Sidereal orb period = 365.25636 d
|
||||||
0)= -3.86
|
Mean daily motion, deg/d = 0.9856474 Hill's sphere radius = 234.9
|
||||||
Solar Constant (W/m^2) = 1367.6 (mean),
|
*******************************************************************************
|
||||||
1414 (perihelion),
|
|
||||||
1322 (aphelion)
|
|
||||||
HELIOCENTRIC ORBIT CHARACTERISTICS:
|
*******************************************************************************
|
||||||
Obliquity to orbit, deg = 23.4392911 Sidereal orb period = 1.0000174 y
|
Ephemeris / API_USER Thu Aug 14 15:51:50 2025 Pasadena, USA / Horizons
|
||||||
Orbital speed, km/s = 29.79 Sidereal orb period = 365.25636 d
|
*******************************************************************************
|
||||||
Mean daily motion, deg/d = 0.9856474 Hill's sphere radius = 234.9
|
Target body name: Earth (399) {source: DE441}
|
||||||
*******************************************************************************
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
*******************************************************************************
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
Ephemeris / API_USER Wed Aug 13 04: 00: 37 2025 Pasadena, USA / Horizons
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
*******************************************************************************
|
Step-size : 1 minutes
|
||||||
Target body name: Earth (399) {source: DE441
|
*******************************************************************************
|
||||||
}
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
Center body name: Sun (10) {source: DE441
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
}
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
Center-site name: BODY CENTER
|
Output units : AU-D
|
||||||
*******************************************************************************
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
Start time : A.D. 2000-Jan-01 12: 00: 00.0000 TDB
|
Output type : GEOMETRIC cartesian states
|
||||||
Stop time : A.D. 2000-Jan-01 12: 01: 00.0000 TDB
|
Output format : 2 (position and velocity)
|
||||||
Step-size : 1 minutes
|
Reference frame : Ecliptic of J2000.0
|
||||||
*******************************************************************************
|
*******************************************************************************
|
||||||
Center geodetic : 0.0,
|
JDTDB
|
||||||
0.0,
|
X Y Z
|
||||||
0.0 {E-lon(deg),Lat(deg),Alt(km)
|
VX VY VZ
|
||||||
}
|
*******************************************************************************
|
||||||
Center cylindric: 0.0,
|
$$SOE
|
||||||
0.0,
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
0.0 {E-lon(deg),Dxy(km),Dz(km)
|
X =-1.786834409731047E-01 Y = 9.669827953774551E-01 Z =-5.109423915082682E-05
|
||||||
}
|
VX=-1.720473858166942E-02 VY=-3.193533189307208E-03 VZ= 5.457174067040888E-09
|
||||||
Center radii : 695700.0,
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
695700.0,
|
X =-1.786953886946605E-01 Y = 9.669805775731443E-01 Z =-5.109423538992340E-05
|
||||||
695700.0 km {Equator_a, b, pole_c
|
VX=-1.720469949887746E-02 VY=-3.193743226004856E-03 VZ= 5.374519991317428E-09
|
||||||
}
|
$$EOE
|
||||||
Output units : AU-D
|
*******************************************************************************
|
||||||
Calendar mode : Mixed Julian/Gregorian
|
|
||||||
Output type : GEOMETRIC cartesian states
|
TIME
|
||||||
Output format : 2 (position and velocity)
|
|
||||||
Reference frame : Ecliptic of J2000.0
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
*******************************************************************************
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
JDTDB
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
X Y Z
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
VX VY VZ
|
variable in the solar system relativistic equations of motion.
|
||||||
*******************************************************************************
|
|
||||||
$$SOE
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
2451545.000000000 = A.D. 2000-Jan-01 12: 00: 00.0000 TDB
|
of irregularities in Earth's rotation.
|
||||||
X =-1.771350992727098E-01 Y = 9.672416867665306E-01 Z =-4.085281582511366E-06
|
|
||||||
VX=-1.720762506872895E-02 VY=-3.158782144324866E-03 VZ= 1.049888594613343E-07
|
CALENDAR SYSTEM
|
||||||
2451545.000694444 = A.D. 2000-Jan-01 12: 01: 00.0000 TDB
|
|
||||||
X =-1.771470489993106E-01 Y = 9.672394930949845E-01 Z =-4.085208640488331E-06
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
VX=-1.720758754114626E-02 VY=-3.158991907845201E-03 VZ= 1.050842029536420E-07
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
$$EOE
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
*******************************************************************************
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
TIME
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
|
||||||
continuous coordinate time is equivalent to the relativistic proper time
|
REFERENCE FRAME AND COORDINATES
|
||||||
of a clock at rest in a reference frame co-moving with the solar system
|
|
||||||
barycenter but outside the system's gravity well. It is the independent
|
Ecliptic at the standard reference epoch
|
||||||
variable in the solar system relativistic equations of motion.
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
TDB runs at a uniform rate of one SI second per second and is independent
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
of irregularities in Earth's rotation.
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
CALENDAR SYSTEM
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
|
||||||
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
are in the Julian calendar system, which is automatically extended for dates
|
|
||||||
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
matching historical dates. The Gregorian calendar more accurately corresponds
|
X X-component of position vector (au)
|
||||||
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
Y Y-component of position vector (au)
|
||||||
available if such physical events are the primary interest.
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
REFERENCE FRAME AND COORDINATES
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
Ecliptic at the standard reference epoch
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
Reference epoch: J2000.0
|
|
||||||
X-Y plane: adopted Earth orbital plane at the reference epoch
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
|
||||||
X-axis : ICRF
|
Computations by ...
|
||||||
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
|
||||||
of Earth's north pole at the reference epoch.
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
Symbol meaning [
|
Pasadena, CA 91109 USA
|
||||||
1 au= 149597870.700 km,
|
|
||||||
1 day= 86400.0 s
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
]:
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
JDTDB Julian Day Number, Barycentric Dynamical Time
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
X X-component of position vector (au)
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
Y Y-component of position vector (au)
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
Z Z-component of position vector (au)
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
VX X-component of velocity vector (au/day)
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
VY Y-component of velocity vector (au/day)
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
VZ Z-component of velocity vector (au/day)
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
ABERRATIONS AND CORRECTIONS
|
|
||||||
|
|
||||||
Geometric state vectors have NO corrections or aberrations applied.
|
|
||||||
|
|
||||||
Computations by ...
|
|
||||||
|
|
||||||
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
|
||||||
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
|
||||||
Pasadena, CA 91109 USA
|
|
||||||
|
|
||||||
General site: https: //ssd.jpl.nasa.gov/
|
|
||||||
Mailing list: https: //ssd.jpl.nasa.gov/email_list.html
|
|
||||||
System news : https: //ssd.jpl.nasa.gov/horizons/news.html
|
|
||||||
User Guide : https: //ssd.jpl.nasa.gov/horizons/manual.html
|
|
||||||
Connect : browser https: //ssd.jpl.nasa.gov/horizons/app.html#/x
|
|
||||||
API https: //ssd-api.jpl.nasa.gov/doc/horizons.html
|
|
||||||
command-line telnet ssd.jpl.nasa.gov 6775
|
|
||||||
e-mail/batch https: //ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
|
||||||
scripts https: //ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
|
||||||
Author : Jon.D.Giorgini@jpl.nasa.gov
|
|
||||||
*******************************************************************************
|
|
||||||
117
assets/jpl_horizon/bodies/Enceladus.txt
Normal file
117
assets/jpl_horizon/bodies/Enceladus.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Enceladus / (Saturn) 602
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 252.3 +- 0.6 Density (g/cm^3) = 1.606 +- 0.012
|
||||||
|
Mass (10^19 kg) = 10.805 Geometric Albedo = 1.04
|
||||||
|
GM (km^3/s^2) = 7.210367 V(1,0) = +2.2
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to local Laplace plane):
|
||||||
|
Semi-major axis, a (km) = 238.04(10^3) Orbital period = 1.370218 d
|
||||||
|
Eccentricity, e = 0.0047 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 0.009
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:41 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Enceladus (602) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.462107070733344E+00 Y =-1.763590731315564E+00 Z =-3.465134777458668E-01
|
||||||
|
VX=-4.799068161710644E-03 VY= 9.904458072213898E-03 VZ=-1.910803547584920E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.462103732792631E+00 Y =-1.763583858405023E+00 Z =-3.465148014677353E-01
|
||||||
|
VX=-4.814191894040593E-03 VY= 9.889516719170488E-03 VZ=-1.901512359359666E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
114
assets/jpl_horizon/bodies/Europa.txt
Normal file
114
assets/jpl_horizon/bodies/Europa.txt
Normal file
@ -0,0 +1,114 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Mar 12, 2021 Europa / (Jupiter) 502
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean radius (km) = 1560.8 +- 0.3 Density (g cm^-3)= 3.013 +- 0.005
|
||||||
|
GM (km^3/s^2) = 3202.7121+- 0.0054 Geometric Albedo = 0.67 +/- 0.03
|
||||||
|
|
||||||
|
SATELLITE ORBIT (at J2000.0 epoch, 2000-Jan-1.5):
|
||||||
|
Semi-major axis, a (km) ~ 671,000 Orbital period ~ 3.55 d
|
||||||
|
Eccentricity, e ~ 0.00981 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) ~ 0.462
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:31 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Europa (502) {source: jup365_merged}
|
||||||
|
Center body name: Sun (10) {source: jup365_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.060479105966296E+00 Y = 4.971193788432235E+00 Z =-4.418907806556983E-02
|
||||||
|
VX=-6.967074192246404E-03 VY= 9.896683771810605E-03 VZ= 4.296001484155991E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.060474264291992E+00 Y = 4.971200661324026E+00 Z =-4.418877980080166E-02
|
||||||
|
VX=-6.976947895835117E-03 VY= 9.897242536020881E-03 VZ= 4.294023144406136E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
114
assets/jpl_horizon/bodies/Ganymede.txt
Normal file
114
assets/jpl_horizon/bodies/Ganymede.txt
Normal file
@ -0,0 +1,114 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Mar 12, 2021 Ganymede / (Jupiter) 503
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean radius (km) = 2631.2 +- 1.7 Density (g cm^-3)= 1.942 +- 0.005
|
||||||
|
GM (km^3/s^2) = 9887.8328+- 0.0074 Geometric Albedo = 0.43 +- 0.02
|
||||||
|
|
||||||
|
SATELLITE ORBIT (at J2000.0 epoch, 2000-Jan-1.5):
|
||||||
|
Semi-major axis, a (km) ~ 1,070,000 Orbital period ~ 7.155 d
|
||||||
|
Eccentricity, e ~ 0.00146 Rotational period= Synchronous
|
||||||
|
Inclination, i (deg) ~ 0.207
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:32 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Ganymede (503) {source: jup365_merged}
|
||||||
|
Center body name: Sun (10) {source: jup365_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.062520398626604E+00 Y = 4.968458682597362E+00 Z =-4.429967587277176E-02
|
||||||
|
VX=-4.841408463186764E-03 VY= 7.634290231598638E-03 VZ= 4.147177169244575E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.062517035324768E+00 Y = 4.968463984744183E+00 Z =-4.429938787030207E-02
|
||||||
|
VX=-4.844900988782714E-03 VY= 7.635892259759473E-03 VZ= 4.147293801627869E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Iapetus.txt
Normal file
117
assets/jpl_horizon/bodies/Iapetus.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Iapetus / (Saturn) 608
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 734.5 +- 4.0 Density (g/cm^3)= 1.088 +- 0.018
|
||||||
|
Mass (10^19 kg) = 180.59 Geometric Albedo= 0.6
|
||||||
|
GM (km^3/s^2) = 120.52 +- 0.03 V(1,0) = +1.5 (.7-2.5)
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean values with respect to local Laplace plane):
|
||||||
|
Semi-major axis, a (km)= 3560.84 (10^3) Orbital period = 79.33 d
|
||||||
|
Eccentricity, e = 0.0283 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 7.489
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:37 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Iapetus (608) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.454548058738080E+00 Y =-1.786906158368561E+00 Z =-3.394196336672040E-01
|
||||||
|
VX= 2.477125925502744E-03 VY= 4.942920731685813E-03 VZ=-3.564738618756286E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.454549778973153E+00 Y =-1.786902725752121E+00 Z =-3.394198812278713E-01
|
||||||
|
VX= 2.477151084385878E-03 VY= 4.943014616239762E-03 VZ=-3.565008602876317E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
114
assets/jpl_horizon/bodies/Io.txt
Normal file
114
assets/jpl_horizon/bodies/Io.txt
Normal file
@ -0,0 +1,114 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Mar 12, 2021 Io / (Jupiter) 501
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean radius (km) = 1821.49 Density (g cm^-3) = 3.528 +- 0.006
|
||||||
|
GM (km^3/s^2) = 5959.9155+- 0.004 Geometric Albedo = 0.63 +- 0.02
|
||||||
|
|
||||||
|
SATELLITE ORBIT (at J2000.0 epoch, 2000-Jan-1.5):
|
||||||
|
Semi-major axis, a (km)~ 422,000 Orbital period ~ 1.77 d
|
||||||
|
Eccentricity, e ~ 0.00472 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) ~ 0.0375
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:30 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Io (501) {source: jup365_merged}
|
||||||
|
Center body name: Sun (10) {source: jup365_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.053815818667817E+00 Y = 4.969715993299296E+00 Z =-4.437108516416628E-02
|
||||||
|
VX=-1.329530996368361E-03 VY=-5.983335980023409E-03 VZ=-3.295420474951598E-05
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.053814902131768E+00 Y = 4.969711843495328E+00 Z =-4.437110776557460E-02
|
||||||
|
VX=-1.310099171031782E-03 VY=-5.968091504155077E-03 VZ=-3.213765991234832E-05
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
125
assets/jpl_horizon/bodies/Jupiter.txt
Normal file
125
assets/jpl_horizon/bodies/Jupiter.txt
Normal file
@ -0,0 +1,125 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: April 12, 2021 Jupiter 599
|
||||||
|
|
||||||
|
PHYSICAL DATA (revised 2025-Jan-30):
|
||||||
|
Mass x 10^26 (kg) = 18.9819 Density (g/cm^3) = 1.3262 +- .0003
|
||||||
|
Equat. radius (1 bar) = 71492+-4 km Polar radius (km) = 66854+-10
|
||||||
|
Vol. Mean Radius (km) = 69911+-6 Flattening = 0.06487
|
||||||
|
Geometric Albedo = 0.52 Rocky core mass (Mc/M)= 0.0261
|
||||||
|
Sid. rot. period (III)= 9h 55m 29.711 s Sid. rot. rate (rad/s)= 0.00017585
|
||||||
|
Mean solar day, hrs = ~9.9259
|
||||||
|
GM (km^3/s^2) = 126686531.900 GM 1-sigma (km^3/s^2) = +- 1.2732
|
||||||
|
Equ. grav, ge (m/s^2) = 24.79 Pol. grav, gp (m/s^2) = 28.34
|
||||||
|
Vis. magnitude V(1,0) = -9.40
|
||||||
|
Vis. mag. (opposition)= -2.70 Obliquity to orbit = 3.13 deg
|
||||||
|
Sidereal orbit period = 11.861982204 y Sidereal orbit period = 4332.589 d
|
||||||
|
Mean daily motion = 0.0831294 deg/d Mean orbit speed, km/s= 13.0697
|
||||||
|
Atmos. temp. (1 bar) = 165+-5 K Escape speed, km/s = 59.5
|
||||||
|
A_roche(ice)/Rp = 2.76 Hill's sphere rad. Rp = 740
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 56 46 51
|
||||||
|
Maximum Planetary IR (W/m^2) 13.7 13.4 13.6
|
||||||
|
Minimum Planetary IR (W/m^2) 13.7 13.4 13.6
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:54 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Jupiter (599) {source: jup365_merged}
|
||||||
|
Center body name: Sun (10) {source: jup365_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.056033545576702E+00 Y = 4.971452162023883E+00 Z =-4.427806378454757E-02
|
||||||
|
VX=-7.476272400979211E-03 VY= 1.924466075080766E-03 VZ= 1.592575331437652E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.056028353720140E+00 Y = 4.971453498455673E+00 Z =-4.427795318902549E-02
|
||||||
|
VX=-7.476274498134918E-03 VY= 1.924457475706055E-03 VZ= 1.592575690535828E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
126
assets/jpl_horizon/bodies/Mars.txt
Normal file
126
assets/jpl_horizon/bodies/Mars.txt
Normal file
@ -0,0 +1,126 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: June 02, 2025 Mars 499 / 4
|
||||||
|
|
||||||
|
PHYSICAL DATA (updated 2025-Jun-02):
|
||||||
|
Vol. mean radius (km) = 3389.92+-0.04 Density (g/cm^3) = 3.933(5+-4)
|
||||||
|
Mass x10^23 (kg) = 6.4171 Flattening, f = 1/169.779
|
||||||
|
Volume (x10^10 km^3) = 16.318 Equatorial radius (km)= 3396.19
|
||||||
|
Sidereal rot. period = 24.622962 hr Sid. rot. rate, rad/s = 0.0000708822
|
||||||
|
Mean solar day (sol) = 88775.24415 s Polar gravity m/s^2 = 3.758
|
||||||
|
Core radius (km) = ~1700 Equ. gravity m/s^2 = 3.71
|
||||||
|
Geometric Albedo = 0.150
|
||||||
|
|
||||||
|
GM (km^3/s^2) = 42828.375662 Mass ratio (Sun/Mars) = 3098703.59
|
||||||
|
GM 1-sigma (km^3/s^2) = +- 0.00028 Mass of atmosphere, kg= ~ 2.5 x 10^16
|
||||||
|
Mean temperature (K) = 210 Atmos. pressure (bar) = 0.0056
|
||||||
|
Obliquity to orbit = 25.19 deg Max. angular diam. = 17.9"
|
||||||
|
Mean sidereal orb per = 1.88081578 y Visual mag. V(1,0) = -1.52
|
||||||
|
Mean sidereal orb per = 686.98 d Orbital speed, km/s = 24.13
|
||||||
|
Hill's sphere rad. Rp = 319.8 Escape speed, km/s = 5.027
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 717 493 589
|
||||||
|
Maximum Planetary IR (W/m^2) 470 315 390
|
||||||
|
Minimum Planetary IR (W/m^2) 30 30 30
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:53 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Mars (499) {source: mar099}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X =-5.216858665681381E-01 Y = 1.525234576802456E+00 Z = 4.475559803760917E-02
|
||||||
|
VX=-1.271183490340250E-02 VY=-3.338839586395265E-03 VZ= 2.417788175776839E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X =-5.216946942223875E-01 Y = 1.525232258137904E+00 Z = 4.475576593880412E-02
|
||||||
|
VX=-1.271180933472031E-02 VY=-3.338914323653169E-03 VZ= 2.417766240577524E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
124
assets/jpl_horizon/bodies/Mercury.txt
Normal file
124
assets/jpl_horizon/bodies/Mercury.txt
Normal file
@ -0,0 +1,124 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: April 12, 2021 Mercury 199 / 1
|
||||||
|
|
||||||
|
PHYSICAL DATA (updated 2024-Mar-04):
|
||||||
|
Vol. Mean Radius (km) = 2439.4+-0.1 Density (g cm^-3) = 5.427
|
||||||
|
Mass x10^23 (kg) = 3.302 Volume (x10^10 km^3) = 6.085
|
||||||
|
Sidereal rot. period = 58.6463 d Sid. rot. rate (rad/s)= 0.00000124001
|
||||||
|
Mean solar day = 175.9421 d Core radius (km) = ~1600
|
||||||
|
Geometric Albedo = 0.106 Surface emissivity = 0.77+-0.06
|
||||||
|
GM (km^3/s^2) = 22031.86855 Equatorial radius, Re = 2440.53 km
|
||||||
|
GM 1-sigma (km^3/s^2) = Mass ratio (Sun/plnt) = 6023682
|
||||||
|
Mom. of Inertia = 0.33 Equ. gravity m/s^2 = 3.701
|
||||||
|
Atmos. pressure (bar) = < 5x10^-15 Max. angular diam. = 11.0"
|
||||||
|
Mean Temperature (K) = 440 Visual mag. V(1,0) = -0.42
|
||||||
|
Obliquity to orbit[1] = 2.11' +/- 0.1' Hill's sphere rad. Rp = 94.4
|
||||||
|
Sidereal orb. per. = 0.2408467 y Mean Orbit vel. km/s = 47.362
|
||||||
|
Sidereal orb. per. = 87.969257 d Escape vel. km/s = 4.435
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 14462 6278 9126
|
||||||
|
Maximum Planetary IR (W/m^2) 12700 5500 8000
|
||||||
|
Minimum Planetary IR (W/m^2) 6 6 6
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:24 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Mercury (199) {source: DE441}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X =-3.873030085256687E-01 Y =-1.617241946342014E-01 Z = 2.230772540124238E-02
|
||||||
|
VX= 5.024430196457658E-03 VY=-2.474345331076241E-02 VZ=-2.482923861184285E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X =-3.872995189658449E-01 Y =-1.617413774324715E-01 Z = 2.230600112712438E-02
|
||||||
|
VX= 5.025502090388155E-03 VY=-2.474300570104969E-02 VZ=-2.482985597610005E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Mimas.txt
Normal file
117
assets/jpl_horizon/bodies/Mimas.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Mimas / (Saturn) 601
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 198.8 +- 1.5 Density (g/cm^3) = 1.152 +- 0.027
|
||||||
|
Mass (10^19 kg) = 3.75 Geometric Albedo = 0.6
|
||||||
|
GM (km^3/s^2) = 2.503489 V(1,0) = +3.3
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to local Laplace plane):
|
||||||
|
Semi-major axis, a (km) = 185.54(10^3) Orbital period = 0.9424218 d
|
||||||
|
Eccentricity, e = 0.0196 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 1.572
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:43 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Mimas (601) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.462113317387443E+00 Y =-1.764120396234732E+00 Z =-3.462575454806998E-01
|
||||||
|
VX=-3.600569225193193E-03 VY= 1.195945377622506E-02 VZ=-3.321658418910402E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.462110805168413E+00 Y =-1.764112096667343E+00 Z =-3.462598478664664E-01
|
||||||
|
VX=-3.634605921905340E-03 VY= 1.194327556531391E-02 VZ=-3.309200303182580E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Miranda.txt
Normal file
115
assets/jpl_horizon/bodies/Miranda.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 29, 2025 Miranda / (Uranus) 705
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 240x234.2x232.9 Density (g cm^-3) = 1.18 +- 0.05
|
||||||
|
GM (km^3/s^2) = 4.3 +- 0.2 Geometric Albedo = 0.27
|
||||||
|
V(1,0) = +3.6
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to equatorial plane & IAU pole)
|
||||||
|
Semi-major axis, a (km) = 129.8 (10^3) Orbital period = 1.413 d
|
||||||
|
Eccentricity, e = 0.0027 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 175.78
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:49 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Miranda (705) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110338075481133E+01 Y = 1.609470886437212E+01 Z =-8.339848717695617E-02
|
||||||
|
VX= 2.787135511093017E-04 VY= 1.302160355796409E-03 VZ= 1.366210183434322E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110338094954377E+01 Y = 1.609470976757570E+01 Z =-8.339754224366069E-02
|
||||||
|
VX= 2.821101872080506E-04 VY= 1.299067156991778E-03 VZ= 1.355195633050134E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
@ -1,127 +1,125 @@
|
|||||||
curl -s "https://ssd.jpl.nasa.gov/api/horizons.api?format=text&COMMAND=%27301%27&CENTER=%27%40sun%27&EPHEM_TYPE=%27VECTORS%27&OUT_UNITS=%27AU-D%27&START_TIME=%272000-01-01%2012:00%27&STOP_TIME=%272000-01-01%2012:01%27&STEP_SIZE=%271%20m%27&VEC_TABLE=2&REF_PLANE=%27ECLIPTIC%27&REF_SYSTEM=%27J2000%27"
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
API VERSION: 1.2
|
|
||||||
API SOURCE: NASA/JPL Horizons API
|
*******************************************************************************
|
||||||
|
Revised: July 31, 2013 Moon / (Earth) 301
|
||||||
*******************************************************************************
|
|
||||||
Revised: July 31, 2013 Moon / (Earth) 301
|
GEOPHYSICAL DATA (updated 2018-Aug-15):
|
||||||
|
Vol. mean radius, km = 1737.53+-0.03 Mass, x10^22 kg = 7.349
|
||||||
GEOPHYSICAL DATA (updated 2018-Aug-15):
|
Radius (gravity), km = 1738.0 Surface emissivity = 0.92
|
||||||
Vol. mean radius, km = 1737.53+-0.03 Mass, x10^22 kg = 7.349
|
Radius (IAU), km = 1737.4 GM, km^3/s^2 = 4902.800066
|
||||||
Radius (gravity), km = 1738.0 Surface emissivity = 0.92
|
Density, g/cm^3 = 3.3437 GM 1-sigma, km^3/s^2 = +-0.0001
|
||||||
Radius (IAU), km = 1737.4 GM, km^3/s^2 = 4902.800066
|
V(1,0) = +0.21 Surface accel., m/s^2 = 1.62
|
||||||
Density, g/cm^3 = 3.3437 GM 1-sigma, km^3/s^2 = +-0.0001
|
Earth/Moon mass ratio = 81.3005690769 Farside crust. thick. = ~80 - 90 km
|
||||||
V(1,0) = +0.21 Surface accel., m/s^2 = 1.62
|
Mean crustal density = 2.97+-.07 g/cm^3 Nearside crust. thick.= 58+-8 km
|
||||||
Earth/Moon mass ratio = 81.3005690769 Farside crust. thick. = ~80 - 90 km
|
Heat flow, Apollo 15 = 3.1+-.6 mW/m^2 Mean angular diameter = 31'05.2"
|
||||||
Mean crustal density = 2.97+-.07 g/cm^3 Nearside crust. thick.= 58+-8 km
|
Heat flow, Apollo 17 = 2.2+-.5 mW/m^2 Sid. rot. rate, rad/s = 0.0000026617
|
||||||
Heat flow, Apollo 15 = 3.1+-.6 mW/m^2 Mean angular diameter = 31'05.2"
|
Geometric Albedo = 0.12 Mean solar day = 29.5306 d
|
||||||
Heat flow, Apollo 17 = 2.2+-.5 mW/m^2 Sid. rot. rate, rad/s = 0.0000026617
|
Obliquity to orbit = 6.67 deg Orbit period = 27.321582 d
|
||||||
Geometric Albedo = 0.12 Mean solar day = 29.5306 d
|
Semi-major axis, a = 384400 km Eccentricity = 0.05490
|
||||||
Obliquity to orbit = 6.67 deg Orbit period = 27.321582 d
|
Mean motion, rad/s = 2.6616995x10^-6 Inclination = 5.145 deg
|
||||||
Semi-major axis, a = 384400 km Eccentricity = 0.05490
|
Apsidal period = 3231.50 d Nodal period = 6798.38 d
|
||||||
Mean motion, rad/s = 2.6616995x10^-6 Inclination = 5.145 deg
|
Perihelion Aphelion Mean
|
||||||
Apsidal period = 3231.50 d Nodal period = 6798.38 d
|
Solar Constant (W/m^2) 1414+-7 1323+-7 1368+-7
|
||||||
Perihelion Aphelion Mean
|
Maximum Planetary IR (W/m^2) 1314 1226 1268
|
||||||
Solar Constant (W/m^2) 1414+-7 1323+-7 1368+-7
|
Minimum Planetary IR (W/m^2) 5.2 5.2 5.2
|
||||||
Maximum Planetary IR (W/m^2) 1314 1226 1268
|
********************************************************************************
|
||||||
Minimum Planetary IR (W/m^2) 5.2 5.2 5.2
|
|
||||||
********************************************************************************
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:51 2025 Pasadena, USA / Horizons
|
||||||
*******************************************************************************
|
*******************************************************************************
|
||||||
Ephemeris / API_USER Wed Aug 13 04:01:18 2025 Pasadena, USA / Horizons
|
Target body name: Moon (301) {source: DE441}
|
||||||
*******************************************************************************
|
Center body name: Sun (10) {source: DE441}
|
||||||
Target body name: Moon (301) {source: DE441}
|
Center-site name: BODY CENTER
|
||||||
Center body name: Sun (10) {source: DE441}
|
*******************************************************************************
|
||||||
Center-site name: BODY CENTER
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
*******************************************************************************
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
Start time : A.D. 2000-Jan-01 12:00:00.0000 TDB
|
Step-size : 1 minutes
|
||||||
Stop time : A.D. 2000-Jan-01 12:01:00.0000 TDB
|
*******************************************************************************
|
||||||
Step-size : 1 minutes
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
*******************************************************************************
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
Output units : AU-D
|
||||||
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
Output units : AU-D
|
Output type : GEOMETRIC cartesian states
|
||||||
Calendar mode : Mixed Julian/Gregorian
|
Output format : 2 (position and velocity)
|
||||||
Output type : GEOMETRIC cartesian states
|
Reference frame : Ecliptic of J2000.0
|
||||||
Output format : 2 (position and velocity)
|
*******************************************************************************
|
||||||
Reference frame : Ecliptic of J2000.0
|
JDTDB
|
||||||
*******************************************************************************
|
X Y Z
|
||||||
JDTDB
|
VX VY VZ
|
||||||
X Y Z
|
*******************************************************************************
|
||||||
VX VY VZ
|
$$SOE
|
||||||
*******************************************************************************
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
$$SOE
|
X =-1.776670337217189E-01 Y = 9.646511868801392E-01 Z =-2.560710414773878E-04
|
||||||
2451545.000000000 = A.D. 2000-Jan-01 12:00:00.0000 TDB
|
VX=-1.666610342674751E-02 VY=-2.935662211368250E-03 VZ= 2.214641479437884E-05
|
||||||
X =-1.790843809223965E-01 Y = 9.654035607264573E-01 Z = 2.383726922995396E-04
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
VX=-1.683595459141215E-02 VY=-3.580960720855671E-03 VZ=-6.540550604528720E-06
|
X =-1.776786074043311E-01 Y = 9.646491481829632E-01 Z =-2.560556593596988E-04
|
||||||
2451545.000694444 = A.D. 2000-Jan-01 12:01:00.0000 TDB
|
VX=-1.666610249864482E-02 VY=-2.935785656373790E-03 VZ= 2.215408427478499E-05
|
||||||
X =-1.790960725225740E-01 Y = 9.654010738956424E-01 Z = 2.383681475637660E-04
|
$$EOE
|
||||||
VX=-1.683585392087164E-02 VY=-3.581112024431721E-03 VZ=-6.548288423082821E-06
|
*******************************************************************************
|
||||||
$$EOE
|
|
||||||
*******************************************************************************
|
TIME
|
||||||
|
|
||||||
TIME
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
continuous coordinate time is equivalent to the relativistic proper time
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
of a clock at rest in a reference frame co-moving with the solar system
|
variable in the solar system relativistic equations of motion.
|
||||||
barycenter but outside the system's gravity well. It is the independent
|
|
||||||
variable in the solar system relativistic equations of motion.
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
TDB runs at a uniform rate of one SI second per second and is independent
|
|
||||||
of irregularities in Earth's rotation.
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
CALENDAR SYSTEM
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
are in the Julian calendar system, which is automatically extended for dates
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
matching historical dates. The Gregorian calendar more accurately corresponds
|
available if such physical events are the primary interest.
|
||||||
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
|
||||||
available if such physical events are the primary interest.
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
REFERENCE FRAME AND COORDINATES
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
Ecliptic at the standard reference epoch
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
Reference epoch: J2000.0
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
X-Y plane: adopted Earth orbital plane at the reference epoch
|
X-axis : ICRF
|
||||||
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
X-axis : ICRF
|
of Earth's north pole at the reference epoch.
|
||||||
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
|
||||||
of Earth's north pole at the reference epoch.
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
JDTDB Julian Day Number, Barycentric Dynamical Time
|
Y Y-component of position vector (au)
|
||||||
X X-component of position vector (au)
|
Z Z-component of position vector (au)
|
||||||
Y Y-component of position vector (au)
|
VX X-component of velocity vector (au/day)
|
||||||
Z Z-component of position vector (au)
|
VY Y-component of velocity vector (au/day)
|
||||||
VX X-component of velocity vector (au/day)
|
VZ Z-component of velocity vector (au/day)
|
||||||
VY Y-component of velocity vector (au/day)
|
|
||||||
VZ Z-component of velocity vector (au/day)
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
ABERRATIONS AND CORRECTIONS
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
Geometric state vectors have NO corrections or aberrations applied.
|
Computations by ...
|
||||||
|
|
||||||
Computations by ...
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
Pasadena, CA 91109 USA
|
||||||
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
|
||||||
Pasadena, CA 91109 USA
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
General site: https://ssd.jpl.nasa.gov/
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
command-line telnet ssd.jpl.nasa.gov 6775
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
*******************************************************************************
|
||||||
Author : Jon.D.Giorgini@jpl.nasa.gov
|
|
||||||
*******************************************************************************
|
|
||||||
125
assets/jpl_horizon/bodies/Neptune.txt
Normal file
125
assets/jpl_horizon/bodies/Neptune.txt
Normal file
@ -0,0 +1,125 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: April 22, 2021 Neptune 899
|
||||||
|
|
||||||
|
PHYSICAL DATA (update 2021-May-03):
|
||||||
|
Mass x10^24 (kg) = 102.409 Density (g/cm^3) = 1.638
|
||||||
|
Equat. radius (1 bar) = 24766+-15 km Volume, 10^10 km^3 = 6254
|
||||||
|
Vol. mean radius (km) = 24624+-21 Polar radius (km) = 24342+-30
|
||||||
|
Geometric Albedo = 0.41 Flattening = 0.0171
|
||||||
|
Sid. rot. period (III)= 16.11+-0.01 hr Sid. rot. rate (rad/s) = 0.000108338
|
||||||
|
Mean solar day, h =~16.11 h
|
||||||
|
GM (km^3/s^2) = 6835099.97 GM 1-sigma (km^3/s^2) = +-10
|
||||||
|
Equ. grav, ge (m/s^2) = 11.15 Pol. grav, gp (m/s^2) = 11.41+-0.03
|
||||||
|
Visual magnitude V(1,0)= -6.87
|
||||||
|
Vis. mag. (opposition)= +7.84 Obliquity to orbit = 28.32 deg
|
||||||
|
Sidereal orbit period = 164.788501027 y Sidereal orbit period = 60189 d
|
||||||
|
Mean daily motion = 0.006020076dg/d Mean orbit velocity = 5.43 km/s
|
||||||
|
Atmos. temp. (1 bar) = 72+-2 K Escape speed (1 bar) = 23.5 km/s
|
||||||
|
Aroche(ice)/Rp = 2.98 Hill's sphere rad., Rp = 4700
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 1.54 1.49 1.51
|
||||||
|
Maximum Planetary IR (W/m^2) 0.52 0.52 0.52
|
||||||
|
Minimum Planetary IR (W/m^2) 0.52 0.52 0.52
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:58 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Neptune (899) {source: nep097_merged}
|
||||||
|
Center body name: Sun (10) {source: nep097_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 2.987992735576156E+01 Y =-6.341879950443392E-01 Z =-6.754997950415415E-01
|
||||||
|
VX= 3.941595250081164E-05 VY= 3.160389775728832E-03 VZ=-6.636996572427530E-05
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 2.987992738313355E+01 Y =-6.341858003292957E-01 Z =-6.754998411317725E-01
|
||||||
|
VX= 3.941539715732043E-05 VY= 3.160389549672231E-03 VZ=-6.636990015457822E-05
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Oberon.txt
Normal file
115
assets/jpl_horizon/bodies/Oberon.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 29, 2025 Oberon / (Uranus) 704
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 761.4 +- 2.6 Density (g cm^-3) = 1.66 +- 0.05
|
||||||
|
GM (km^3/s^2) = 205.34 +- 5.8 Geometric Albedo = 0.24
|
||||||
|
V(1,0) = +1.23
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to equatorial plane & IAU pole)
|
||||||
|
Semi-major axis, a (km) = 582.6 (10^3) Orbital period = 13.463 d
|
||||||
|
Eccentricity, e = 0.0008 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 179.90
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:45 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Oberon (704) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110301190463219E+01 Y = 1.609515778477002E+01 Z =-8.040210462613612E-02
|
||||||
|
VX=-1.519780917379062E-03 VY= 1.720169702110850E-03 VZ= 3.926675849694972E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110301084926093E+01 Y = 1.609515897929689E+01 Z =-8.040183213898029E-02
|
||||||
|
VX=-1.519688343927354E-03 VY= 1.720067705450287E-03 VZ= 3.920954185698925E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Phobos.txt
Normal file
115
assets/jpl_horizon/bodies/Phobos.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jun 02, 2025 Phobos / (Mars) 401
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 13.1 x11.1 x9.3 Density (g cm^-3) = 1.90 +- 0.08
|
||||||
|
Mass (10^20 kg ) = 1.08 (10^-4) Geometric Albedo = 0.06
|
||||||
|
(+- 0.1) V(1,0) = +11.8
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA:
|
||||||
|
Semi-major axis, a (km) = 9.3772(10^3) Orbital period = 0.319 d
|
||||||
|
Eccentricity, e = 0.0151 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 1.082
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:27 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Phobos (401) {source: mar099}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X =-5.216607506283159E-01 Y = 1.525290094552813E+00 Z = 4.474552444674667E-02
|
||||||
|
VX=-1.371531677510715E-02 VY=-2.797359927923991E-03 VZ= 7.604209362929195E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X =-5.216702775783473E-01 Y = 1.525288146474805E+00 Z = 4.474605348954465E-02
|
||||||
|
VX=-1.372226672058481E-02 VY=-2.813122639161171E-03 VZ= 7.632054629505637E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Rhea.txt
Normal file
117
assets/jpl_horizon/bodies/Rhea.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Rhea / (Saturn) 605
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 764.5 +- 2 Density (g/cm^3) = 1.233 +- 0.010
|
||||||
|
Mass (10^19 kg) = 230.9 Geometric Albedo = 0.6
|
||||||
|
GM (km^3/s^2) = 153.94 +- 0.16 V(1,0) = +0.1
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean values referred to local Laplace plane):
|
||||||
|
Semi-major axis, a (km) = 527.07(10^3) Orbital period = 4.518 d
|
||||||
|
Eccentricity, e = 0.001 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 0.331
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:36 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Rhea (605) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.463441058546145E+00 Y =-1.766997606737125E+00 Z =-3.448366300385151E-01
|
||||||
|
VX= 4.307393238751094E-03 VY= 8.273257376182423E-03 VZ=-1.932435874857194E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.463444048680545E+00 Y =-1.766991860305545E+00 Z =-3.448379724938126E-01
|
||||||
|
VX= 4.304193275713166E-03 VY= 8.276465140546280E-03 VZ=-1.933835100794230E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
125
assets/jpl_horizon/bodies/Saturn.txt
Normal file
125
assets/jpl_horizon/bodies/Saturn.txt
Normal file
@ -0,0 +1,125 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: January 26, 2022 Saturn 699
|
||||||
|
|
||||||
|
PHYSICAL DATA:
|
||||||
|
Mass x10^26 (kg) = 5.6834 Density (g/cm^3) = 0.687+-.001
|
||||||
|
Equat. radius (1 bar) = 60268+-4 km Polar radius (km) = 54364+-10
|
||||||
|
Vol. Mean Radius (km) = 58232+-6 Flattening = 0.09796
|
||||||
|
Geometric Albedo = 0.47 Rocky core mass (Mc/M) = 0.1027
|
||||||
|
Sid. rot. period (III)= 10h 39m 22.4s Sid. rot. rate (rad/s) = 0.000163785
|
||||||
|
Mean solar day, hrs =~10.656
|
||||||
|
GM (km^3/s^2) = 37931206.234 GM 1-sigma (km^3/s^2) = +- 98
|
||||||
|
Equ. grav, ge (m/s^2) = 10.44 Pol. grav, gp (m/s^2) = 12.14+-0.01
|
||||||
|
Vis. magnitude V(1,0) = -8.88
|
||||||
|
Vis. mag. (opposition)= +0.67 Obliquity to orbit = 26.73 deg
|
||||||
|
Sidereal orbit period = 29.447498 yr Sidereal orbit period = 10755.698 d
|
||||||
|
Mean daily motion = 0.0334979 deg/d Mean orbit velocity = 9.68 km/s
|
||||||
|
Atmos. temp. (1 bar) = 134+-4 K Escape speed, km/s = 35.5
|
||||||
|
Aroche(ice)/Rp = 2.71 Hill's sphere rad. Rp = 1100
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 16.8 13.6 15.1
|
||||||
|
Maximum Planetary IR (W/m^2) 4.7 4.5 4.6
|
||||||
|
Minimum Planetary IR (W/m^2) 4.7 4.5 4.6
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:55 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Saturn (699) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.461067271500818E+00 Y =-1.764614720843175E+00 Z =-3.458764004169705E-01
|
||||||
|
VX= 7.093807804551229E-04 VY= 5.475097536527790E-03 VZ=-1.232345969963958E-04
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.461067764125684E+00 Y =-1.764610918691946E+00 Z =-3.458764859965446E-01
|
||||||
|
VX= 7.093788338554797E-04 VY= 5.475098004312488E-03 VZ=-1.232345764512067E-04
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
@ -1,126 +1,124 @@
|
|||||||
curl -s "https://ssd.jpl.nasa.gov/api/horizons.api?format=text&COMMAND=%27%40sun%27&CENTER=%27%40sun%27&EPHEM_TYPE=%27VECTORS%27&OUT_UNITS=%27AU-D%27&START_TIME=%272000-01-01%2012:00%27&STOP_TIME=%272000-01-01%2012:01%27&STEP_SIZE=%271%20m%27&VEC_TABLE=2&REF_PLANE=%27ECLIPTIC%27&REF_SYSTEM=%27J2000%27"
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
API VERSION: 1.2
|
|
||||||
API SOURCE: NASA/JPL Horizons API
|
*******************************************************************************
|
||||||
|
Revised: July 31, 2013 Sun 10
|
||||||
*******************************************************************************
|
|
||||||
Revised: July 31, 2013 Sun 10
|
PHYSICAL PROPERTIES (updated 2024-Oct-30):
|
||||||
|
GM, km^3/s^2 = 132712440041.93938 Mass, 10^24 kg = ~1988410
|
||||||
PHYSICAL PROPERTIES (updated 2024-Oct-30):
|
Vol. mean radius, km = 695700 Volume, 10^12 km^3 = 1412000
|
||||||
GM, km^3/s^2 = 132712440041.93938 Mass, 10^24 kg = ~1988410
|
Solar radius (IAU2015)= 695700 km Mean density, g/cm^3 = 1.408
|
||||||
Vol. mean radius, km = 695700 Volume, 10^12 km^3 = 1412000
|
Radius (photosphere) = 696500 km Angular diam at 1 AU = 1919.3"
|
||||||
Solar radius (IAU2015)= 695700 km Mean density, g/cm^3 = 1.408
|
Photosphere temp., K = 6600 (bottom) Photosphere temp., K = 4400(top)
|
||||||
Radius (photosphere) = 696500 km Angular diam at 1 AU = 1919.3"
|
Photospheric depth = ~500 km Chromospheric depth = ~2500 km
|
||||||
Photosphere temp., K = 6600 (bottom) Photosphere temp., K = 4400(top)
|
Flatness, f = 0.00005 Adopted sid. rot. per.= 25.38 d
|
||||||
Photospheric depth = ~500 km Chromospheric depth = ~2500 km
|
Surface gravity = 274.0 m/s^2 Escape speed, km/s = 617.7
|
||||||
Flatness, f = 0.00005 Adopted sid. rot. per.= 25.38 d
|
Pole (RA,DEC), deg. = (286.13, 63.87) Obliquity to ecliptic = 7.25 deg.
|
||||||
Surface gravity = 274.0 m/s^2 Escape speed, km/s = 617.7
|
Solar constant (1 AU) = 1367.6 W/m^2 Luminosity, 10^24 J/s = 382.8
|
||||||
Pole (RA,DEC), deg. = (286.13, 63.87) Obliquity to ecliptic = 7.25 deg.
|
Mass-energy conv rate = 4.260 x 10^9 kg/s Effective temp, K = 5772
|
||||||
Solar constant (1 AU) = 1367.6 W/m^2 Luminosity, 10^24 J/s = 382.8
|
Sunspot cycle = 11.4 yr Cycle 24 sunspot min. = 2008 A.D.
|
||||||
Mass-energy conv rate = 4.260 x 10^9 kg/s Effective temp, K = 5772
|
|
||||||
Sunspot cycle = 11.4 yr Cycle 24 sunspot min. = 2008 A.D.
|
Motion relative to nearby stars = apex : R.A.= 271 deg.; DEC.= +30 deg.
|
||||||
|
speed: 19.4 km/s (0.0112 au/day)
|
||||||
Motion relative to nearby stars = apex : R.A.= 271 deg.; DEC.= +30 deg.
|
Motion relative to 2.73K BB/CBR = apex : l= 264.7 +- 0.8; b= 48.2 +- 0.5 deg.
|
||||||
speed: 19.4 km/s (0.0112 au/day)
|
speed: 369 +-11 km/s
|
||||||
Motion relative to 2.73K BB/CBR = apex : l= 264.7 +- 0.8; b= 48.2 +- 0.5 deg.
|
*******************************************************************************
|
||||||
speed: 369 +-11 km/s
|
|
||||||
*******************************************************************************
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:49 2025 Pasadena, USA / Horizons
|
||||||
*******************************************************************************
|
*******************************************************************************
|
||||||
Ephemeris / API_USER Wed Aug 13 04:05:18 2025 Pasadena, USA / Horizons
|
Target body name: Sun (10) {source: DE441}
|
||||||
*******************************************************************************
|
Center body name: Sun (10) {source: DE441}
|
||||||
Target body name: Sun (10) {source: DE441}
|
Center-site name: BODY CENTER
|
||||||
Center body name: Sun (10) {source: DE441}
|
*******************************************************************************
|
||||||
Center-site name: BODY CENTER
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
*******************************************************************************
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
Start time : A.D. 2000-Jan-01 12:00:00.0000 TDB
|
Step-size : 1 minutes
|
||||||
Stop time : A.D. 2000-Jan-01 12:01:00.0000 TDB
|
*******************************************************************************
|
||||||
Step-size : 1 minutes
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
*******************************************************************************
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
Output units : AU-D
|
||||||
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
Output units : AU-D
|
Output type : GEOMETRIC cartesian states
|
||||||
Calendar mode : Mixed Julian/Gregorian
|
Output format : 2 (position and velocity)
|
||||||
Output type : GEOMETRIC cartesian states
|
Reference frame : Ecliptic of J2000.0
|
||||||
Output format : 2 (position and velocity)
|
*******************************************************************************
|
||||||
Reference frame : Ecliptic of J2000.0
|
JDTDB
|
||||||
*******************************************************************************
|
X Y Z
|
||||||
JDTDB
|
VX VY VZ
|
||||||
X Y Z
|
*******************************************************************************
|
||||||
VX VY VZ
|
$$SOE
|
||||||
*******************************************************************************
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
$$SOE
|
X = 0.000000000000000E+00 Y = 0.000000000000000E+00 Z = 0.000000000000000E+00
|
||||||
2451545.000000000 = A.D. 2000-Jan-01 12:00:00.0000 TDB
|
VX= 0.000000000000000E+00 VY= 0.000000000000000E+00 VZ= 0.000000000000000E+00
|
||||||
X = 0.000000000000000E+00 Y = 0.000000000000000E+00 Z = 0.000000000000000E+00
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
VX= 0.000000000000000E+00 VY= 0.000000000000000E+00 VZ= 0.000000000000000E+00
|
X = 0.000000000000000E+00 Y = 0.000000000000000E+00 Z = 0.000000000000000E+00
|
||||||
2451545.000694444 = A.D. 2000-Jan-01 12:01:00.0000 TDB
|
VX= 0.000000000000000E+00 VY= 0.000000000000000E+00 VZ= 0.000000000000000E+00
|
||||||
X = 0.000000000000000E+00 Y = 0.000000000000000E+00 Z = 0.000000000000000E+00
|
$$EOE
|
||||||
VX= 0.000000000000000E+00 VY= 0.000000000000000E+00 VZ= 0.000000000000000E+00
|
*******************************************************************************
|
||||||
$$EOE
|
|
||||||
*******************************************************************************
|
TIME
|
||||||
|
|
||||||
TIME
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
continuous coordinate time is equivalent to the relativistic proper time
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
of a clock at rest in a reference frame co-moving with the solar system
|
variable in the solar system relativistic equations of motion.
|
||||||
barycenter but outside the system's gravity well. It is the independent
|
|
||||||
variable in the solar system relativistic equations of motion.
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
TDB runs at a uniform rate of one SI second per second and is independent
|
|
||||||
of irregularities in Earth's rotation.
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
CALENDAR SYSTEM
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
are in the Julian calendar system, which is automatically extended for dates
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
matching historical dates. The Gregorian calendar more accurately corresponds
|
available if such physical events are the primary interest.
|
||||||
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
|
||||||
available if such physical events are the primary interest.
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
REFERENCE FRAME AND COORDINATES
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
Ecliptic at the standard reference epoch
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
Reference epoch: J2000.0
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
X-Y plane: adopted Earth orbital plane at the reference epoch
|
X-axis : ICRF
|
||||||
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
X-axis : ICRF
|
of Earth's north pole at the reference epoch.
|
||||||
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
|
||||||
of Earth's north pole at the reference epoch.
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
JDTDB Julian Day Number, Barycentric Dynamical Time
|
Y Y-component of position vector (au)
|
||||||
X X-component of position vector (au)
|
Z Z-component of position vector (au)
|
||||||
Y Y-component of position vector (au)
|
VX X-component of velocity vector (au/day)
|
||||||
Z Z-component of position vector (au)
|
VY Y-component of velocity vector (au/day)
|
||||||
VX X-component of velocity vector (au/day)
|
VZ Z-component of velocity vector (au/day)
|
||||||
VY Y-component of velocity vector (au/day)
|
|
||||||
VZ Z-component of velocity vector (au/day)
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
ABERRATIONS AND CORRECTIONS
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
Geometric state vectors have NO corrections or aberrations applied.
|
Computations by ...
|
||||||
|
|
||||||
Computations by ...
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
Pasadena, CA 91109 USA
|
||||||
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
|
||||||
Pasadena, CA 91109 USA
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
General site: https://ssd.jpl.nasa.gov/
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
command-line telnet ssd.jpl.nasa.gov 6775
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
*******************************************************************************
|
||||||
Author : Jon.D.Giorgini@jpl.nasa.gov
|
|
||||||
*******************************************************************************
|
|
||||||
117
assets/jpl_horizon/bodies/Tethys.txt
Normal file
117
assets/jpl_horizon/bodies/Tethys.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Tethys / (Saturn) 603
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 536.3 +- 1.5 Density (g/cm^3) = 0.956+- 0.008
|
||||||
|
Mass (10^19 kg) = 61.76 +- 0.11 Geometric Albedo = 0.80
|
||||||
|
GM (km^3/s^2) = 41.21 +- 0.007 V(1,0) = +0.7
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean values with respect to local Laplace plane):
|
||||||
|
Semi-major axis, a (km)= 294.670(10^3) Orbital period = 1.888 d
|
||||||
|
Eccentricity, e = 0.0001 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 1.091
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:40 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Tethys (603) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.463028141754283E+00 Y =-1.764725184828637E+00 Z =-3.460263238634043E-01
|
||||||
|
VX= 8.124741088132637E-04 VY= 1.132977234261396E-02 VZ=-3.072248079372077E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.463028700733389E+00 Y =-1.764717316639481E+00 Z =-3.460284569666105E-01
|
||||||
|
VX= 7.973856311297915E-04 VY= 1.133060721568177E-02 VZ=-3.071086528742641E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Titan.txt
Normal file
117
assets/jpl_horizon/bodies/Titan.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 26, 2022 Titan / (Saturn) 606
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_phys_par
|
||||||
|
http://ssd.jpl.nasa.gov/?sat_elem
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean Radius (km) = 2575.5 +- 2.0 Density (g/cm^3) = 1.880 +- 0.004
|
||||||
|
Mass (10^19 kg) = 13455.3 Geometric Albedo = 0.2
|
||||||
|
GM (km^3/s^2) = 8978.14 +- 0.06 V(1,0) = -1.2
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA:
|
||||||
|
Semi-major axis, a (km)= 1221.87 (10^3) Orbital period = 15.945421 d
|
||||||
|
Eccentricity, e = 0.0288 Rotational period =
|
||||||
|
Inclination, i (deg) = 0.28
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:35 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Titan (606) {source: sat441l}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 9.468440328490537E+00 Y =-1.762284834421733E+00 Z =-3.478122131916790E-01
|
||||||
|
VX=-4.611400435334967E-04 VY= 8.260265884102586E-03 VZ=-1.443082816825538E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 9.468440007956742E+00 Y =-1.762279098219692E+00 Z =-3.478132152545299E-01
|
||||||
|
VX=-4.619972666944876E-04 VY= 8.259995958078317E-03 VZ=-1.442858176376882E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Titania.txt
Normal file
115
assets/jpl_horizon/bodies/Titania.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 29, 2025 Titania / (Uranus) 703
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 788.9 +- 1.8 Density (g cm^-3) = 1.65 +- 0.03
|
||||||
|
GM (km^3/s^2) = 222.8 +- 4.1 Geometric Albedo = 0.27
|
||||||
|
V(1,0) = +1.02
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to equatorial plane & IAU pole)
|
||||||
|
Semi-major axis, a (km) = 435.8 (10^3) Orbital period = 8.706 d
|
||||||
|
Eccentricity, e = 0.0022 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 179.90
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:44 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Titania (703) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110510884778205E+01 Y = 1.609382177197045E+01 Z =-8.661833178512783E-02
|
||||||
|
VX=-5.032495225759578E-03 VY= 2.280002002691279E-03 VZ=-1.088327315015861E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110510535280710E+01 Y = 1.609382335538846E+01 Z =-8.661908726294103E-02
|
||||||
|
VX=-5.033032537876168E-03 VY= 2.280241869921879E-03 VZ=-1.087448734649130E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
117
assets/jpl_horizon/bodies/Triton.txt
Normal file
117
assets/jpl_horizon/bodies/Triton.txt
Normal file
@ -0,0 +1,117 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Apr 22, 2021 Triton / (Neptune) 801
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Mean radius (km) = 1352.6 +- 2.4 Mean dens (g cm^-3)= 2.065 +-0.011
|
||||||
|
GM (km^3/s^2) = 1428.495 +- 0.62 Geometric Albedo = 0.7
|
||||||
|
V(1,0) = -1.24
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean values wrt Laplace plane):
|
||||||
|
Semi-major axis, a (km) = 354800 Orbital period = 5.876994 d
|
||||||
|
Eccentricity, e = 0.000 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 157.3
|
||||||
|
|
||||||
|
Fit to all reported measurements through 2020 (Voyager 2, ground, HST)
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:50 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Triton (801) {source: nep097_merged}
|
||||||
|
Center body name: Sun (10) {source: nep097_merged}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 2.987802053077272E+01 Y =-6.355569689698364E-01 Z =-6.751627943073906E-01
|
||||||
|
VX=-6.787804924900204E-04 VY= 4.636375429506899E-03 VZ= 1.865945736548040E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 2.987802005992279E+01 Y =-6.355537488875286E-01 Z =-6.751614986047274E-01
|
||||||
|
VX=-6.772672129266950E-04 VY= 4.637461481841197E-03 VZ= 1.865677756098451E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
115
assets/jpl_horizon/bodies/Umbriel.txt
Normal file
115
assets/jpl_horizon/bodies/Umbriel.txt
Normal file
@ -0,0 +1,115 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: Jan 29, 2025 Umbriel / (Uranus) 702
|
||||||
|
|
||||||
|
SATELLITE PHYSICAL PROPERTIES:
|
||||||
|
Radius (km) = 584.7 +- 2.8 Density (g cm^-3) = 1.52 +- 0.04
|
||||||
|
GM (km^3/s^2) = 85.40 +- 1.9 Geometric Albedo = 0.18
|
||||||
|
V(1,0) = +2.10
|
||||||
|
|
||||||
|
SATELLITE ORBITAL DATA (mean elements referred to equatorial plane & IAU pole):
|
||||||
|
Semi-major axis, a (km) = 266.0 (10^3) Orbital period = 4.144 d
|
||||||
|
Eccentricity, e = 0.0050 Rotational period = Synchronous
|
||||||
|
Inclination, i (deg) = 179.64
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:48 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Umbriel (702) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110253678329407E+01 Y = 1.609490555702174E+01 Z =-8.286998450094619E-02
|
||||||
|
VX=-1.219602563560983E-03 VY= 1.849034126664038E-03 VZ= 1.801100761916168E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110253593696041E+01 Y = 1.609490684083643E+01 Z =-8.286873448230965E-02
|
||||||
|
VX=-1.217838766094139E-03 VY= 1.848352214682835E-03 VZ= 1.798952584612123E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
125
assets/jpl_horizon/bodies/Uranus.txt
Normal file
125
assets/jpl_horizon/bodies/Uranus.txt
Normal file
@ -0,0 +1,125 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: January 29, 2025 Uranus 799
|
||||||
|
|
||||||
|
PHYSICAL DATA:
|
||||||
|
Mass x10^24 (kg) = 86.813 Density (g/cm^3) = 1.271
|
||||||
|
Equat. radius (1 bar) = 25559+-4 km Polar radius (km) = 24973+-20
|
||||||
|
Vol. Mean Radius (km) = 25362+-12 Flattening = 0.02293
|
||||||
|
Geometric Albedo = 0.51
|
||||||
|
Sid. rot. period (III)= 17.24+-0.01 h Sid. rot. rate (rad/s) = -0.000101237
|
||||||
|
Mean solar day, h =~17.24 Rocky core mass (Mc/M) = 0.0012
|
||||||
|
GM (km^3/s^2) = 5793950.6103 GM 1-sigma (km^3/s^2) = +-4.3
|
||||||
|
Equ. grav, ge (m/s^2) = 8.87 Pol. grav, gp (m/s^2) = 9.19+-0.02
|
||||||
|
Visual magnitude V(1,0)= -7.11
|
||||||
|
Vis. mag. (opposition)= +5.52 Obliquity to orbit = 97.77 deg
|
||||||
|
Sidereal orbit period = 84.0120465 y Sidereal orbit period = 30685.4 d
|
||||||
|
Mean daily motion = 0.01176904 dg/d Mean orbit velocity = 6.8 km/s
|
||||||
|
Atmos. temp. (1 bar) = 76+-2 K Escape speed, km/s = 21.3
|
||||||
|
Aroche(ice)/Rp = 2.20 Hill's sphere rad., Rp = 2700
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 4.09 3.39 3.71
|
||||||
|
Maximum Planetary IR (W/m^2) 0.72 0.55 0.63
|
||||||
|
Minimum Planetary IR (W/m^2) 0.72 0.55 0.63
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 15:51:56 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Uranus (799) {source: ura183_merged}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 1.110362881512566E+01 Y = 1.609448391218202E+01 Z =-8.419833258524990E-02
|
||||||
|
VX=-3.273728238819980E-03 VY= 2.053528328895527E-03 VZ= 5.008589052969062E-05
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 1.110362654170318E+01 Y = 1.609448533824320E+01 Z =-8.419829780338954E-02
|
||||||
|
VX=-3.273728502372206E-03 VY= 2.053527864185684E-03 VZ= 5.008586714126605E-05
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
124
assets/jpl_horizon/bodies/Venus.txt
Normal file
124
assets/jpl_horizon/bodies/Venus.txt
Normal file
@ -0,0 +1,124 @@
|
|||||||
|
API VERSION: 1.2
|
||||||
|
API SOURCE: NASA/JPL Horizons API
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Revised: April 12, 2021 Venus 299 / 2
|
||||||
|
|
||||||
|
PHYSICAL DATA (updated 2020-Oct-19):
|
||||||
|
Vol. Mean Radius (km) = 6051.84+-0.01 Density (g/cm^3) = 5.204
|
||||||
|
Mass x10^23 (kg) = 48.685 Volume (x10^10 km^3) = 92.843
|
||||||
|
Sidereal rot. period = 243.018484 d Sid. Rot. Rate (rad/s)= -0.00000029924
|
||||||
|
Mean solar day = 116.7490 d Equ. gravity m/s^2 = 8.870
|
||||||
|
Mom. of Inertia = 0.33 Core radius (km) = ~3200
|
||||||
|
Geometric Albedo = 0.65 Potential Love # k2 = ~0.25
|
||||||
|
GM (km^3/s^2) = 324858.592 Equatorial Radius, Re = 6051.893 km
|
||||||
|
GM 1-sigma (km^3/s^2) = +-0.006 Mass ratio (Sun/Venus)= 408523.72
|
||||||
|
Atmos. pressure (bar) = 90 Max. angular diam. = 60.2"
|
||||||
|
Mean Temperature (K) = 735 Visual mag. V(1,0) = -4.40
|
||||||
|
Obliquity to orbit = 177.3 deg Hill's sphere rad.,Rp = 167.1
|
||||||
|
Sidereal orb. per., y = 0.61519726 Orbit speed, km/s = 35.021
|
||||||
|
Sidereal orb. per., d = 224.70079922 Escape speed, km/s = 10.361
|
||||||
|
Perihelion Aphelion Mean
|
||||||
|
Solar Constant (W/m^2) 2759 2614 2650
|
||||||
|
Maximum Planetary IR (W/m^2) 153 153 153
|
||||||
|
Minimum Planetary IR (W/m^2) 153 153 153
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
|
||||||
|
*******************************************************************************
|
||||||
|
Ephemeris / API_USER Thu Aug 14 16:19:26 2025 Pasadena, USA / Horizons
|
||||||
|
*******************************************************************************
|
||||||
|
Target body name: Venus (299) {source: DE441}
|
||||||
|
Center body name: Sun (10) {source: DE441}
|
||||||
|
Center-site name: BODY CENTER
|
||||||
|
*******************************************************************************
|
||||||
|
Start time : A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
Stop time : A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
Step-size : 1 minutes
|
||||||
|
*******************************************************************************
|
||||||
|
Center geodetic : 0.0, 0.0, 0.0 {E-lon(deg),Lat(deg),Alt(km)}
|
||||||
|
Center cylindric: 0.0, 0.0, 0.0 {E-lon(deg),Dxy(km),Dz(km)}
|
||||||
|
Center radii : 695700.0, 695700.0, 695700.0 km {Equator_a, b, pole_c}
|
||||||
|
Output units : AU-D
|
||||||
|
Calendar mode : Mixed Julian/Gregorian
|
||||||
|
Output type : GEOMETRIC cartesian states
|
||||||
|
Output format : 2 (position and velocity)
|
||||||
|
Reference frame : Ecliptic of J2000.0
|
||||||
|
*******************************************************************************
|
||||||
|
JDTDB
|
||||||
|
X Y Z
|
||||||
|
VX VY VZ
|
||||||
|
*******************************************************************************
|
||||||
|
$$SOE
|
||||||
|
2460676.500000000 = A.D. 2025-Jan-01 00:00:00.0000 TDB
|
||||||
|
X = 4.534187654737982E-01 Y = 5.622160792960551E-01 Z =-1.844136025242647E-02
|
||||||
|
VX=-1.580627428004959E-02 VY= 1.261006264179427E-02 VZ= 1.085217883057661E-03
|
||||||
|
2460676.500694444 = A.D. 2025-Jan-01 00:01:00.0000 TDB
|
||||||
|
X = 4.534077888086579E-01 Y = 5.622248361776391E-01 Z =-1.844060662540785E-02
|
||||||
|
VX=-1.580652132279067E-02 VY= 1.260975631877725E-02 VZ= 1.085227930639264E-03
|
||||||
|
$$EOE
|
||||||
|
*******************************************************************************
|
||||||
|
|
||||||
|
TIME
|
||||||
|
|
||||||
|
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
|
||||||
|
continuous coordinate time is equivalent to the relativistic proper time
|
||||||
|
of a clock at rest in a reference frame co-moving with the solar system
|
||||||
|
barycenter but outside the system's gravity well. It is the independent
|
||||||
|
variable in the solar system relativistic equations of motion.
|
||||||
|
|
||||||
|
TDB runs at a uniform rate of one SI second per second and is independent
|
||||||
|
of irregularities in Earth's rotation.
|
||||||
|
|
||||||
|
CALENDAR SYSTEM
|
||||||
|
|
||||||
|
Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
|
||||||
|
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
|
||||||
|
are in the Julian calendar system, which is automatically extended for dates
|
||||||
|
prior to its adoption on 45-Jan-1 BC. The Julian calendar is useful for
|
||||||
|
matching historical dates. The Gregorian calendar more accurately corresponds
|
||||||
|
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
|
||||||
|
available if such physical events are the primary interest.
|
||||||
|
|
||||||
|
REFERENCE FRAME AND COORDINATES
|
||||||
|
|
||||||
|
Ecliptic at the standard reference epoch
|
||||||
|
|
||||||
|
Reference epoch: J2000.0
|
||||||
|
X-Y plane: adopted Earth orbital plane at the reference epoch
|
||||||
|
Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
|
||||||
|
X-axis : ICRF
|
||||||
|
Z-axis : perpendicular to the X-Y plane in the directional (+ or -) sense
|
||||||
|
of Earth's north pole at the reference epoch.
|
||||||
|
|
||||||
|
Symbol meaning [1 au= 149597870.700 km, 1 day= 86400.0 s]:
|
||||||
|
|
||||||
|
JDTDB Julian Day Number, Barycentric Dynamical Time
|
||||||
|
X X-component of position vector (au)
|
||||||
|
Y Y-component of position vector (au)
|
||||||
|
Z Z-component of position vector (au)
|
||||||
|
VX X-component of velocity vector (au/day)
|
||||||
|
VY Y-component of velocity vector (au/day)
|
||||||
|
VZ Z-component of velocity vector (au/day)
|
||||||
|
|
||||||
|
ABERRATIONS AND CORRECTIONS
|
||||||
|
|
||||||
|
Geometric state vectors have NO corrections or aberrations applied.
|
||||||
|
|
||||||
|
Computations by ...
|
||||||
|
|
||||||
|
Solar System Dynamics Group, Horizons On-Line Ephemeris System
|
||||||
|
4800 Oak Grove Drive, Jet Propulsion Laboratory
|
||||||
|
Pasadena, CA 91109 USA
|
||||||
|
|
||||||
|
General site: https://ssd.jpl.nasa.gov/
|
||||||
|
Mailing list: https://ssd.jpl.nasa.gov/email_list.html
|
||||||
|
System news : https://ssd.jpl.nasa.gov/horizons/news.html
|
||||||
|
User Guide : https://ssd.jpl.nasa.gov/horizons/manual.html
|
||||||
|
Connect : browser https://ssd.jpl.nasa.gov/horizons/app.html#/x
|
||||||
|
API https://ssd-api.jpl.nasa.gov/doc/horizons.html
|
||||||
|
command-line telnet ssd.jpl.nasa.gov 6775
|
||||||
|
e-mail/batch https://ssd.jpl.nasa.gov/ftp/ssd/horizons_batch.txt
|
||||||
|
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
|
||||||
|
Author : Jon.D.Giorgini@jpl.nasa.gov
|
||||||
|
*******************************************************************************
|
||||||
2992
assets/jpl_horizon/major_bodies.ron
Normal file
2992
assets/jpl_horizon/major_bodies.ron
Normal file
File diff suppressed because it is too large
Load Diff
BIN
assets/models/ariel.glb
Normal file
BIN
assets/models/ariel.glb
Normal file
Binary file not shown.
BIN
assets/models/callisto.glb
Normal file
BIN
assets/models/callisto.glb
Normal file
Binary file not shown.
BIN
assets/models/ceres.glb
Normal file
BIN
assets/models/ceres.glb
Normal file
Binary file not shown.
BIN
assets/models/charon.glb
Normal file
BIN
assets/models/charon.glb
Normal file
Binary file not shown.
BIN
assets/models/deimos.glb
Normal file
BIN
assets/models/deimos.glb
Normal file
Binary file not shown.
BIN
assets/models/dione.glb
Normal file
BIN
assets/models/dione.glb
Normal file
Binary file not shown.
BIN
assets/models/earth.glb
Normal file
BIN
assets/models/earth.glb
Normal file
Binary file not shown.
BIN
assets/models/enceladus.glb
Normal file
BIN
assets/models/enceladus.glb
Normal file
Binary file not shown.
BIN
assets/models/eris.glb
Normal file
BIN
assets/models/eris.glb
Normal file
Binary file not shown.
BIN
assets/models/europa.glb
Normal file
BIN
assets/models/europa.glb
Normal file
Binary file not shown.
BIN
assets/models/ganymede.glb
Normal file
BIN
assets/models/ganymede.glb
Normal file
Binary file not shown.
BIN
assets/models/hubble.glb
Normal file
BIN
assets/models/hubble.glb
Normal file
Binary file not shown.
BIN
assets/models/iapetus.glb
Normal file
BIN
assets/models/iapetus.glb
Normal file
Binary file not shown.
BIN
assets/models/io.glb
Normal file
BIN
assets/models/io.glb
Normal file
Binary file not shown.
BIN
assets/models/iss.glb
Normal file
BIN
assets/models/iss.glb
Normal file
Binary file not shown.
BIN
assets/models/jupiter.glb
Normal file
BIN
assets/models/jupiter.glb
Normal file
Binary file not shown.
BIN
assets/models/makemake.glb
Normal file
BIN
assets/models/makemake.glb
Normal file
Binary file not shown.
BIN
assets/models/mars.glb
Normal file
BIN
assets/models/mars.glb
Normal file
Binary file not shown.
BIN
assets/models/mercury.glb
Normal file
BIN
assets/models/mercury.glb
Normal file
Binary file not shown.
BIN
assets/models/mimas.glb
Normal file
BIN
assets/models/mimas.glb
Normal file
Binary file not shown.
BIN
assets/models/miranda.glb
Normal file
BIN
assets/models/miranda.glb
Normal file
Binary file not shown.
BIN
assets/models/moon.glb
Normal file
BIN
assets/models/moon.glb
Normal file
Binary file not shown.
BIN
assets/models/neptune.glb
Normal file
BIN
assets/models/neptune.glb
Normal file
Binary file not shown.
BIN
assets/models/oberon.glb
Normal file
BIN
assets/models/oberon.glb
Normal file
Binary file not shown.
BIN
assets/models/phobos.glb
Normal file
BIN
assets/models/phobos.glb
Normal file
Binary file not shown.
BIN
assets/models/pluto.glb
Normal file
BIN
assets/models/pluto.glb
Normal file
Binary file not shown.
BIN
assets/models/rhea.glb
Normal file
BIN
assets/models/rhea.glb
Normal file
Binary file not shown.
BIN
assets/models/saturn.glb
Normal file
BIN
assets/models/saturn.glb
Normal file
Binary file not shown.
BIN
assets/models/sun.glb
Normal file
BIN
assets/models/sun.glb
Normal file
Binary file not shown.
BIN
assets/models/tethys.glb
Normal file
BIN
assets/models/tethys.glb
Normal file
Binary file not shown.
BIN
assets/models/titan.glb
Normal file
BIN
assets/models/titan.glb
Normal file
Binary file not shown.
BIN
assets/models/titania.glb
Normal file
BIN
assets/models/titania.glb
Normal file
Binary file not shown.
BIN
assets/models/triton.glb
Normal file
BIN
assets/models/triton.glb
Normal file
Binary file not shown.
BIN
assets/models/umbriel.glb
Normal file
BIN
assets/models/umbriel.glb
Normal file
Binary file not shown.
BIN
assets/models/uranus.glb
Normal file
BIN
assets/models/uranus.glb
Normal file
Binary file not shown.
BIN
assets/models/venus.glb
Normal file
BIN
assets/models/venus.glb
Normal file
Binary file not shown.
BIN
assets/models/voyager.glb
Normal file
BIN
assets/models/voyager.glb
Normal file
Binary file not shown.
30
assets/scale.txt
Normal file
30
assets/scale.txt
Normal file
@ -0,0 +1,30 @@
|
|||||||
|
Applied scale to Deimos: 3.572769492e-5, 2.336041507e-5, 2.748284533e-5
|
||||||
|
Applied scale to Umbriel: 3.375767119e-5, 3.375767119e-5, 3.375767119e-5
|
||||||
|
Applied scale to Phobos: 3.111071419e-5, 2.177749957e-5, 2.728170512e-5
|
||||||
|
Applied scale to Titania: 4.554716361e-5, 4.554716361e-5, 4.554716361e-5
|
||||||
|
Applied scale to Oberon: 4.395945143e-5, 4.395945143e-5, 4.395945143e-5
|
||||||
|
Applied scale to Mercury: 1.409040560e-4, 1.407730015e-4, 1.409040560e-4
|
||||||
|
Applied scale to Callisto: 1.391587430e-4, 1.391587430e-4, 1.391587430e-4
|
||||||
|
Applied scale to Venus: 3.494008561e-4, 3.494008561e-4, 3.494008561e-4
|
||||||
|
Applied scale to Uranus: 1.486925757e-3, 1.452834462e-3, 1.486925757e-3
|
||||||
|
Applied scale to Ariel: 3.354982618e-5, 3.335352449e-5, 3.336507143e-5
|
||||||
|
Applied scale to Europa: 9.021675214e-5, 9.003777086e-5, 9.008396592e-5
|
||||||
|
Applied scale to Pluto: 6.860653230e-5, 6.860653230e-5, 6.860653230e-5
|
||||||
|
Applied scale to Enceladus: 1.481480831e-5, 1.433560737e-5, 1.451458593e-5
|
||||||
|
Applied scale to Dione: 3.252791430e-5, 3.230852235e-5, 3.240667138e-5
|
||||||
|
Applied scale to Titan: 1.486763649e-4, 1.486371038e-4, 1.486549882e-4
|
||||||
|
Applied scale to Miranda: 1.387950124e-5, 1.344648808e-5, 1.352154413e-5
|
||||||
|
Applied scale to Neptune: 1.437890343e-3, 1.413329272e-3, 1.437890343e-3
|
||||||
|
Applied scale to Moon: 1.003505604e-4, 1.003505604e-4, 1.003505604e-4
|
||||||
|
Applied scale to Rhea: 4.416729644e-5, 4.401718616e-5, 4.405760046e-5
|
||||||
|
Applied scale to Sol: 4.016625881e-2, 4.016625881e-2, 4.016625881e-2
|
||||||
|
Applied scale to Iapetus: 4.305300899e-5, 4.111311500e-5, 4.305300899e-5
|
||||||
|
Applied scale to Jupiter: 4.216764122e-3, 3.943203948e-3, 4.216764122e-3
|
||||||
|
Applied scale to Ganymede: 1.519124053e-4, 1.519124053e-4, 1.519124053e-4
|
||||||
|
Applied scale to Earth: 3.686534474e-4, 3.674174368e-4, 3.686534474e-4
|
||||||
|
Applied scale to Saturn: 1.828302280e-3, 1.649197191e-3, 1.828302280e-3
|
||||||
|
Applied scale to Mimas: 3.022084638e-5, 2.771941035e-5, 2.860654604e-5
|
||||||
|
Applied scale to Triton: 7.809240196e-5, 7.809240196e-5, 7.809240196e-5
|
||||||
|
Applied scale to Mars: 1.964640105e-4, 1.953076135e-4, 1.964640105e-4
|
||||||
|
Applied scale to Tethys: 3.129428660e-5, 3.059098162e-5, 3.070722960e-5
|
||||||
|
Applied scale to Io: 1.056204637e-4, 1.048294944e-4, 1.050431092e-4
|
||||||
154
examples/big_space.rs
Normal file
154
examples/big_space.rs
Normal file
@ -0,0 +1,154 @@
|
|||||||
|
//! This example demonstrates what floating point error in rendering looks like. You can press
|
||||||
|
//! space bar to smoothly switch between enabling and disabling the floating origin.
|
||||||
|
//!
|
||||||
|
//! Instead of disabling the plugin outright, this example simply moves the floating origin
|
||||||
|
//! independently of the camera, which is equivalent to what would happen when moving far from the
|
||||||
|
//! origin when not using this plugin.
|
||||||
|
|
||||||
|
use bevy::prelude::*;
|
||||||
|
use big_space::prelude::*;
|
||||||
|
|
||||||
|
fn main() {
|
||||||
|
App::new()
|
||||||
|
.add_plugins((
|
||||||
|
DefaultPlugins.build().disable::<TransformPlugin>(),
|
||||||
|
BigSpaceDefaultPlugins,
|
||||||
|
))
|
||||||
|
.add_systems(Startup, (setup_scene, setup_ui))
|
||||||
|
.add_systems(Update, (rotator_system, toggle_plugin))
|
||||||
|
.run();
|
||||||
|
}
|
||||||
|
|
||||||
|
/// You can put things really, really far away from the origin. The distance we use here is actually
|
||||||
|
/// quite small, because we want the mesh to still be visible when the floating origin is far from
|
||||||
|
/// the camera. If you go much further than this, the mesh will simply disappear in a *POOF* of
|
||||||
|
/// floating point error when we disable this plugin.
|
||||||
|
///
|
||||||
|
/// This plugin can function much further from the origin without any issues. Try setting this to:
|
||||||
|
/// `10_000_000_000_000_000` with the default i64 feature, or
|
||||||
|
/// `10_000_000_000_000_000_000_000_000_000_000_000_000` with the i128 feature.
|
||||||
|
const DISTANCE: GridPrecision = 2_000_000;
|
||||||
|
|
||||||
|
/// Move the floating origin back to the "true" origin when the user presses the spacebar to emulate
|
||||||
|
/// disabling the plugin. Normally you would make your active camera the floating origin to avoid
|
||||||
|
/// this issue.
|
||||||
|
fn toggle_plugin(
|
||||||
|
input: Res<ButtonInput<KeyCode>>,
|
||||||
|
grids: Grids,
|
||||||
|
mut text: Query<&mut Text>,
|
||||||
|
mut disabled: Local<bool>,
|
||||||
|
mut floating_origin: Query<(Entity, &mut CellCoord), With<FloatingOrigin>>,
|
||||||
|
) -> Result {
|
||||||
|
if input.just_pressed(KeyCode::Space) {
|
||||||
|
*disabled = !*disabled;
|
||||||
|
}
|
||||||
|
|
||||||
|
let this_grid = grids
|
||||||
|
.parent_grid(floating_origin.single().unwrap().0)
|
||||||
|
.unwrap();
|
||||||
|
|
||||||
|
let mut origin_cell = floating_origin.single_mut()?.1;
|
||||||
|
let index_max = DISTANCE / this_grid.cell_edge_length() as GridPrecision;
|
||||||
|
let increment = index_max / 100;
|
||||||
|
|
||||||
|
let msg = if *disabled {
|
||||||
|
if origin_cell.x > 0 {
|
||||||
|
origin_cell.x = 0.max(origin_cell.x - increment);
|
||||||
|
origin_cell.y = 0.max(origin_cell.y - increment);
|
||||||
|
origin_cell.z = 0.max(origin_cell.z - increment);
|
||||||
|
|
||||||
|
"Disabling..."
|
||||||
|
} else {
|
||||||
|
"Floating Origin Disabled"
|
||||||
|
}
|
||||||
|
} else if origin_cell.x < index_max {
|
||||||
|
origin_cell.x = index_max.min(origin_cell.x.saturating_add(increment));
|
||||||
|
origin_cell.y = index_max.min(origin_cell.y.saturating_add(increment));
|
||||||
|
origin_cell.z = index_max.min(origin_cell.z.saturating_add(increment));
|
||||||
|
"Enabling..."
|
||||||
|
} else {
|
||||||
|
"Floating Origin Enabled"
|
||||||
|
};
|
||||||
|
|
||||||
|
let dist =
|
||||||
|
index_max.saturating_sub(origin_cell.x) * this_grid.cell_edge_length() as GridPrecision;
|
||||||
|
|
||||||
|
let thousands = |num: GridPrecision| {
|
||||||
|
num.to_string()
|
||||||
|
.as_bytes()
|
||||||
|
.rchunks(3)
|
||||||
|
.rev()
|
||||||
|
.map(core::str::from_utf8)
|
||||||
|
.collect::<Result<Vec<&str>, _>>()
|
||||||
|
.unwrap()
|
||||||
|
.join(",") // separator
|
||||||
|
};
|
||||||
|
|
||||||
|
text.single_mut()?.0 = format!(
|
||||||
|
"Press Spacebar to toggle: {msg}\nCamera distance to floating origin: {}\nMesh distance from origin: {}",
|
||||||
|
thousands(dist),
|
||||||
|
thousands(DISTANCE)
|
||||||
|
);
|
||||||
|
|
||||||
|
Ok(())
|
||||||
|
}
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct Rotator;
|
||||||
|
|
||||||
|
fn rotator_system(time: Res<Time>, mut query: Query<&mut Transform, With<Rotator>>) {
|
||||||
|
for mut transform in &mut query {
|
||||||
|
transform.rotate_y(time.delta_secs());
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
fn setup_ui(mut commands: Commands) {
|
||||||
|
commands.spawn((
|
||||||
|
Text::default(),
|
||||||
|
TextFont {
|
||||||
|
font_size: 30.0,
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
Node {
|
||||||
|
position_type: PositionType::Absolute,
|
||||||
|
top: Val::Px(12.0),
|
||||||
|
left: Val::Px(12.0),
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
));
|
||||||
|
}
|
||||||
|
|
||||||
|
fn setup_scene(mut commands: Commands, asset_server: Res<AssetServer>) {
|
||||||
|
commands.spawn_big_space_default(|root| {
|
||||||
|
let d = DISTANCE / root.grid().cell_edge_length() as GridPrecision;
|
||||||
|
let distant_grid_cell = CellCoord::new(d, d, d);
|
||||||
|
|
||||||
|
// Normally, we would put the floating origin on the camera. However in this example, we
|
||||||
|
// want to show what happens as the camera is far from the origin, to emulate what
|
||||||
|
// happens when this plugin isn't used.
|
||||||
|
root.spawn_spatial((distant_grid_cell, FloatingOrigin));
|
||||||
|
|
||||||
|
root.spawn_spatial((
|
||||||
|
SceneRoot(asset_server.load("models/low_poly_spaceship/scene.gltf#Scene0")),
|
||||||
|
Transform::from_scale(Vec3::splat(0.2)),
|
||||||
|
distant_grid_cell,
|
||||||
|
Rotator,
|
||||||
|
))
|
||||||
|
.with_child((
|
||||||
|
SceneRoot(asset_server.load("models/low_poly_spaceship/scene.gltf#Scene0")),
|
||||||
|
Transform::from_xyz(0.0, 0.0, 20.0),
|
||||||
|
));
|
||||||
|
// light
|
||||||
|
root.spawn_spatial((
|
||||||
|
DirectionalLight::default(),
|
||||||
|
Transform::from_xyz(4.0, -10.0, -4.0),
|
||||||
|
distant_grid_cell,
|
||||||
|
));
|
||||||
|
// camera
|
||||||
|
root.spawn_spatial((
|
||||||
|
Camera3d::default(),
|
||||||
|
Transform::from_xyz(8.0, 8.0, 0.0).looking_at(Vec3::ZERO, Vec3::Y),
|
||||||
|
distant_grid_cell,
|
||||||
|
));
|
||||||
|
});
|
||||||
|
}
|
||||||
87
examples/cam_follow.rs
Normal file
87
examples/cam_follow.rs
Normal file
@ -0,0 +1,87 @@
|
|||||||
|
//! Demonstrates how to have the camera follow a target object
|
||||||
|
|
||||||
|
use bevy::prelude::*;
|
||||||
|
use bevy_panorbit_camera::{PanOrbitCamera, PanOrbitCameraPlugin};
|
||||||
|
use std::f32::consts::TAU;
|
||||||
|
|
||||||
|
fn main() {
|
||||||
|
App::new()
|
||||||
|
.add_plugins(DefaultPlugins)
|
||||||
|
.add_plugins(PanOrbitCameraPlugin)
|
||||||
|
.add_systems(Startup, setup)
|
||||||
|
.add_systems(Update, (animate_cube, cam_follow).chain())
|
||||||
|
.run();
|
||||||
|
}
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct Cube;
|
||||||
|
|
||||||
|
fn setup(
|
||||||
|
mut commands: Commands,
|
||||||
|
mut meshes: ResMut<Assets<Mesh>>,
|
||||||
|
mut materials: ResMut<Assets<StandardMaterial>>,
|
||||||
|
) {
|
||||||
|
// Ground
|
||||||
|
commands.spawn((
|
||||||
|
Mesh3d(meshes.add(Plane3d::default().mesh().size(0.5, 0.5))),
|
||||||
|
MeshMaterial3d(materials.add(Color::srgb(0.3, 0.5, 0.3))),
|
||||||
|
));
|
||||||
|
// Cube
|
||||||
|
commands
|
||||||
|
.spawn((
|
||||||
|
Mesh3d(meshes.add(Cuboid::new(0.1, 0.1, 0.1))),
|
||||||
|
MeshMaterial3d(materials.add(Color::srgb(0.8, 0.7, 0.6))),
|
||||||
|
Transform::from_xyz(0.0, 0.5, 0.0),
|
||||||
|
))
|
||||||
|
.insert(Cube);
|
||||||
|
// Light
|
||||||
|
commands.spawn((
|
||||||
|
PointLight {
|
||||||
|
shadows_enabled: true,
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
Transform::from_xyz(4.0, 8.0, 4.0),
|
||||||
|
));
|
||||||
|
// Camera
|
||||||
|
commands.spawn((
|
||||||
|
Transform::from_translation(Vec3::new(0.0, 0.15, 0.5)),
|
||||||
|
PanOrbitCamera {
|
||||||
|
// Panning the camera changes the focus, and so you most likely want to disable
|
||||||
|
// panning when setting the focus manually
|
||||||
|
pan_sensitivity: 0.0,
|
||||||
|
// If you want to fully control the camera's focus, set smoothness to 0 so it
|
||||||
|
// immediately snaps to that location. If you want the 'follow' to be smoothed,
|
||||||
|
// leave this at default or set it to something between 0 and 1.
|
||||||
|
pan_smoothness: 0.0,
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
));
|
||||||
|
}
|
||||||
|
|
||||||
|
/// Move the cube in a circle around the Y axis
|
||||||
|
fn animate_cube(
|
||||||
|
time: Res<Time>,
|
||||||
|
mut cube_q: Query<&mut Transform, With<Cube>>,
|
||||||
|
mut angle: Local<f32>,
|
||||||
|
) {
|
||||||
|
if let Ok(mut cube_tfm) = cube_q.single_mut() {
|
||||||
|
// Rotate 20 degrees a second, wrapping around to 0 after a full rotation
|
||||||
|
*angle += 20f32.to_radians() * time.delta_secs() % TAU;
|
||||||
|
// Convert angle to position
|
||||||
|
let pos = Vec3::new(angle.sin() * 0.15, 0.05, angle.cos() * 0.15);
|
||||||
|
cube_tfm.translation = pos;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
/// Set the camera's focus to the cube's position
|
||||||
|
fn cam_follow(mut pan_orbit_q: Query<&mut PanOrbitCamera>, cube_q: Query<&Transform, With<Cube>>) {
|
||||||
|
if let Ok(mut pan_orbit) = pan_orbit_q.single_mut() {
|
||||||
|
if let Ok(cube_tfm) = cube_q.single() {
|
||||||
|
pan_orbit.target_focus = cube_tfm.translation;
|
||||||
|
// Whenever changing properties manually like this, it's necessary to force
|
||||||
|
// PanOrbitCamera to update this frame (by default it only updates when there are
|
||||||
|
// input events).
|
||||||
|
pan_orbit.force_update = true;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
98
examples/model.rs
Normal file
98
examples/model.rs
Normal file
@ -0,0 +1,98 @@
|
|||||||
|
use bevy::{
|
||||||
|
core_pipeline::{bloom::Bloom, tonemapping::Tonemapping},
|
||||||
|
prelude::*,
|
||||||
|
window::WindowMode,
|
||||||
|
};
|
||||||
|
use bevy_inspector_egui::{bevy_egui::EguiPlugin, quick::WorldInspectorPlugin};
|
||||||
|
use bevy_panorbit_camera::{PanOrbitCamera, PanOrbitCameraPlugin};
|
||||||
|
use solar_sim::InitialState;
|
||||||
|
|
||||||
|
fn camera(mut commands: Commands) {
|
||||||
|
commands.spawn((
|
||||||
|
PanOrbitCamera {
|
||||||
|
focus: Vec3::new(0., 0.0, 0.0),
|
||||||
|
zoom_lower_limit: SCALE,
|
||||||
|
radius: Some(SCALE * 10.),
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
Camera {
|
||||||
|
hdr: true,
|
||||||
|
clear_color: ClearColorConfig::Custom(Color::BLACK),
|
||||||
|
..default()
|
||||||
|
},
|
||||||
|
Projection::Perspective(PerspectiveProjection {
|
||||||
|
near: 1e-9, // Very close near plane for extreme zooming
|
||||||
|
..default()
|
||||||
|
}),
|
||||||
|
Tonemapping::TonyMcMapface,
|
||||||
|
Bloom::NATURAL,
|
||||||
|
));
|
||||||
|
|
||||||
|
commands.spawn(DirectionalLight {
|
||||||
|
shadows_enabled: true,
|
||||||
|
illuminance: 50_000.0,
|
||||||
|
..default()
|
||||||
|
});
|
||||||
|
}
|
||||||
|
|
||||||
|
const SCALE: f32 = 1.;
|
||||||
|
|
||||||
|
fn setup(mut commands: Commands, asset_server: Res<AssetServer>) {
|
||||||
|
// Load initial state from RON file
|
||||||
|
let initial_state_content = match std::fs::read_to_string("assets/initial_state.ron") {
|
||||||
|
Ok(content) => content,
|
||||||
|
Err(err) => {
|
||||||
|
error!("Failed to read initial_state.ron: {}", err);
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
};
|
||||||
|
|
||||||
|
let initial_state: InitialState = match ron::from_str(&initial_state_content) {
|
||||||
|
Ok(state) => state,
|
||||||
|
Err(err) => {
|
||||||
|
error!("Failed to parse initial_state.ron: {}", err);
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
};
|
||||||
|
|
||||||
|
initial_state
|
||||||
|
.bodies
|
||||||
|
.iter()
|
||||||
|
.enumerate()
|
||||||
|
.for_each(|(i, body)| {
|
||||||
|
commands
|
||||||
|
.spawn(Transform::from_translation(Vec3::new(
|
||||||
|
(i) as f32 * SCALE * 10 as f32,
|
||||||
|
0.,
|
||||||
|
0.,
|
||||||
|
)))
|
||||||
|
.with_children(|parent| {
|
||||||
|
let scene = asset_server.load(format!("models/{}#Scene0", body.model.path));
|
||||||
|
parent.spawn((
|
||||||
|
SceneRoot(scene),
|
||||||
|
Transform::from_scale(Vec3::new(
|
||||||
|
body.model.scale.0,
|
||||||
|
body.model.scale.1,
|
||||||
|
body.model.scale.2,
|
||||||
|
)),
|
||||||
|
));
|
||||||
|
});
|
||||||
|
});
|
||||||
|
}
|
||||||
|
|
||||||
|
fn main() {
|
||||||
|
App::new()
|
||||||
|
.add_plugins(DefaultPlugins.set(WindowPlugin {
|
||||||
|
primary_window: Some(Window {
|
||||||
|
title: "Solar Sim".to_string(),
|
||||||
|
mode: WindowMode::BorderlessFullscreen(MonitorSelection::Primary),
|
||||||
|
..default()
|
||||||
|
}),
|
||||||
|
..default()
|
||||||
|
}))
|
||||||
|
.add_plugins(EguiPlugin::default())
|
||||||
|
.add_plugins(WorldInspectorPlugin::new())
|
||||||
|
.add_plugins(PanOrbitCameraPlugin)
|
||||||
|
.add_systems(Startup, (camera, setup))
|
||||||
|
.run();
|
||||||
|
}
|
||||||
2329
src/jpl_horizon.rs
Normal file
2329
src/jpl_horizon.rs
Normal file
File diff suppressed because it is too large
Load Diff
23
src/lib.rs
Normal file
23
src/lib.rs
Normal file
@ -0,0 +1,23 @@
|
|||||||
|
use serde::Deserialize;
|
||||||
|
|
||||||
|
// Data structures for deserializing initial_state.ron
|
||||||
|
#[derive(Deserialize)]
|
||||||
|
pub struct InitialState {
|
||||||
|
pub bodies: Vec<CelestialBodyData>,
|
||||||
|
}
|
||||||
|
|
||||||
|
#[derive(Deserialize)]
|
||||||
|
pub struct CelestialBodyData {
|
||||||
|
pub name: String,
|
||||||
|
pub mass: f64, // kg
|
||||||
|
pub radius: f64, // km
|
||||||
|
pub position: (f64, f64, f64), // AU
|
||||||
|
pub velocity: (f64, f64, f64), // AU/day
|
||||||
|
pub model: ModelInfo,
|
||||||
|
}
|
||||||
|
|
||||||
|
#[derive(Deserialize)]
|
||||||
|
pub struct ModelInfo {
|
||||||
|
pub path: String,
|
||||||
|
pub scale: (f32, f32, f32),
|
||||||
|
}
|
||||||
597
src/main.rs
597
src/main.rs
@ -2,46 +2,50 @@ use bevy::{
|
|||||||
core_pipeline::{bloom::Bloom, tonemapping::Tonemapping},
|
core_pipeline::{bloom::Bloom, tonemapping::Tonemapping},
|
||||||
math::DVec3,
|
math::DVec3,
|
||||||
prelude::*,
|
prelude::*,
|
||||||
window::WindowMode,
|
window::{WindowMode, WindowResolution},
|
||||||
};
|
};
|
||||||
use bevy_inspector_egui::{bevy_egui::EguiPlugin, quick::WorldInspectorPlugin};
|
use bevy_inspector_egui::{bevy_egui::EguiPlugin, quick::WorldInspectorPlugin};
|
||||||
use bevy_panorbit_camera::{PanOrbitCamera, PanOrbitCameraPlugin};
|
use bevy_panorbit_camera::{PanOrbitCamera, PanOrbitCameraPlugin};
|
||||||
|
use iyes_perf_ui::{PerfUiPlugin, prelude::*};
|
||||||
|
use solar_sim::InitialState;
|
||||||
|
|
||||||
|
mod jpl_horizon;
|
||||||
|
|
||||||
// Scaling factor to convert AU to game units
|
// Scaling factor to convert AU to game units
|
||||||
// Neptune is approximately 30.1 astronomical units (AU) from the Sun
|
// Neptune is approximately 30.1 astronomical units (AU) from the Sun
|
||||||
// Point light effective range is about 10 game units, so 10 game units = ~30 AU
|
// Point light effective range is about 10 game units, so 10 game units = ~30 AU
|
||||||
const AU_TO_GAME_UNITS: f64 = 0.3;
|
const AU_TO_GAME_UNITS: f64 = 1. / 3.;
|
||||||
|
|
||||||
// Unit wrapper types - all distances in AU
|
// Unit wrapper types - all distances in AU
|
||||||
#[derive(Clone, Copy, Debug, PartialEq)]
|
#[derive(Clone, Copy, Debug, PartialEq, Reflect)]
|
||||||
pub struct DistanceAu(pub f64);
|
pub struct DistanceAu(pub f64);
|
||||||
|
|
||||||
#[derive(Clone, Copy, Debug, PartialEq)]
|
#[derive(Clone, Copy, Debug, PartialEq, Reflect)]
|
||||||
pub struct PositionAu(pub DVec3);
|
pub struct PositionAu(pub DVec3);
|
||||||
|
|
||||||
#[derive(Clone, Copy, Debug, PartialEq)]
|
#[derive(Clone, Copy, Debug, PartialEq, Reflect)]
|
||||||
pub struct VelocityAuPerDay(pub DVec3);
|
pub struct VelocityAuPerDay(pub DVec3);
|
||||||
|
|
||||||
#[derive(Clone, Copy, Debug, PartialEq)]
|
#[derive(Clone, Copy, Debug, PartialEq, Reflect)]
|
||||||
pub struct MassKg(pub f64);
|
pub struct MassSolarMass(pub f64);
|
||||||
|
|
||||||
#[derive(Clone, Debug, PartialEq)]
|
#[derive(Clone, Debug, PartialEq, Reflect)]
|
||||||
pub struct ObjectName(pub String);
|
pub struct ObjectName(pub String);
|
||||||
|
|
||||||
// Component wrappers
|
// Component wrappers
|
||||||
#[derive(Component)]
|
#[derive(Component, Reflect)]
|
||||||
struct Position(PositionAu);
|
struct Position(PositionAu);
|
||||||
|
|
||||||
#[derive(Component)]
|
#[derive(Component, Reflect)]
|
||||||
struct Velocity(VelocityAuPerDay);
|
struct Velocity(VelocityAuPerDay);
|
||||||
|
|
||||||
#[derive(Component)]
|
#[derive(Component, Reflect)]
|
||||||
struct Mass(MassKg);
|
struct Mass(MassSolarMass);
|
||||||
|
|
||||||
#[derive(Component)]
|
#[derive(Component, Reflect)]
|
||||||
struct Radius(DistanceAu);
|
struct Radius(DistanceAu);
|
||||||
|
|
||||||
#[derive(Component)]
|
#[derive(Component, Reflect)]
|
||||||
struct Name(ObjectName);
|
struct Name(ObjectName);
|
||||||
|
|
||||||
#[derive(Bundle)]
|
#[derive(Bundle)]
|
||||||
@ -56,92 +60,75 @@ struct ObjectBundle {
|
|||||||
#[derive(Component)]
|
#[derive(Component)]
|
||||||
struct Star;
|
struct Star;
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct EmissiveEnhanced;
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct NeedsEmissiveEnhancement;
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct EmissiveEnhancementAttempts {
|
||||||
|
attempts: u32,
|
||||||
|
max_attempts: u32,
|
||||||
|
}
|
||||||
|
|
||||||
|
#[derive(Component)]
|
||||||
|
struct Earth;
|
||||||
|
|
||||||
// Component for UI name labels
|
// Component for UI name labels
|
||||||
#[derive(Component)]
|
#[derive(Component)]
|
||||||
struct ObjectLabel {
|
struct ObjectLabel {
|
||||||
target_entity: Entity,
|
target_entity: Entity,
|
||||||
}
|
}
|
||||||
|
|
||||||
|
// Component to control label visibility
|
||||||
|
#[derive(Component)]
|
||||||
|
struct LabelVisible(bool);
|
||||||
|
|
||||||
// Component to mark objects that can be focused on with proper zoom levels
|
// Component to mark objects that can be focused on with proper zoom levels
|
||||||
#[derive(Component)]
|
#[derive(Component)]
|
||||||
struct Trackable {}
|
struct Trackable {}
|
||||||
|
|
||||||
|
#[derive(Resource)]
|
||||||
|
struct Origin {
|
||||||
|
target: Option<Entity>,
|
||||||
|
}
|
||||||
|
|
||||||
pub struct SolarRenderingPlugin;
|
pub struct SolarRenderingPlugin;
|
||||||
|
|
||||||
impl Plugin for SolarRenderingPlugin {
|
impl Plugin for SolarRenderingPlugin {
|
||||||
fn build(&self, app: &mut App) {
|
fn build(&self, app: &mut App) {
|
||||||
app.add_systems(Startup, (setup_rendering, setup_ui))
|
app.insert_resource(Origin { target: None })
|
||||||
|
.add_systems(Startup, (setup_rendering, setup_ui))
|
||||||
.add_systems(
|
.add_systems(
|
||||||
FixedPostUpdate,
|
FixedPostUpdate,
|
||||||
(
|
(
|
||||||
sync_radius_to_mesh,
|
|
||||||
sync_position_to_transform,
|
sync_position_to_transform,
|
||||||
sync_name_labels,
|
sync_name_labels,
|
||||||
|
manage_label_overlaps
|
||||||
|
.after(sync_position_to_transform)
|
||||||
|
.after(sync_name_labels),
|
||||||
),
|
),
|
||||||
)
|
)
|
||||||
.add_systems(Update, (update_label_positions, handle_label_clicks));
|
.add_systems(
|
||||||
}
|
PostUpdate,
|
||||||
}
|
(update_label_positions.after(manage_label_overlaps),),
|
||||||
|
)
|
||||||
fn sync_radius_to_mesh(
|
.add_systems(Update, (handle_label_clicks, handle_speed_controls));
|
||||||
mut commands: Commands,
|
|
||||||
mut meshes: ResMut<Assets<Mesh>>,
|
|
||||||
mut materials: ResMut<Assets<StandardMaterial>>,
|
|
||||||
query: Query<(Entity, &Radius, Option<&Star>, Option<&Mesh3d>), Changed<Radius>>,
|
|
||||||
) {
|
|
||||||
for (entity, radius, star, existing_mesh) in query.iter() {
|
|
||||||
// Convert AU to game units for rendering
|
|
||||||
let render_radius = radius.0.0 * AU_TO_GAME_UNITS;
|
|
||||||
|
|
||||||
println!("render_radius: {:?}", render_radius);
|
|
||||||
|
|
||||||
// Create or update sphere mesh
|
|
||||||
let sphere_mesh = meshes.add(Sphere::new(render_radius as f32));
|
|
||||||
let material = materials.add(if star.is_none() {
|
|
||||||
StandardMaterial {
|
|
||||||
base_color: Color::WHITE,
|
|
||||||
..default()
|
|
||||||
}
|
|
||||||
} else {
|
|
||||||
StandardMaterial {
|
|
||||||
base_color: Color::WHITE, // Sun-like color for stars
|
|
||||||
emissive: LinearRgba::rgb(200.0, 200.0, 200.0),
|
|
||||||
..default()
|
|
||||||
}
|
|
||||||
});
|
|
||||||
|
|
||||||
if existing_mesh.is_none() {
|
|
||||||
// Add mesh and material components if they don't exist
|
|
||||||
commands
|
|
||||||
.entity(entity)
|
|
||||||
.insert((Mesh3d(sphere_mesh), MeshMaterial3d(material)));
|
|
||||||
} else {
|
|
||||||
// Update existing mesh
|
|
||||||
commands.entity(entity).insert(Mesh3d(sphere_mesh));
|
|
||||||
}
|
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
fn sync_position_to_transform(
|
fn sync_position_to_transform(
|
||||||
mut commands: Commands,
|
mut query: Query<(Entity, &Position, &mut Transform)>,
|
||||||
mut query: Query<(Entity, &Position, Option<&mut Transform>), Changed<Position>>,
|
origin: Res<Origin>,
|
||||||
) {
|
) {
|
||||||
for (entity, position, transform) in query.iter_mut() {
|
let offset = origin.target.map_or(DVec3::ZERO, |target| {
|
||||||
// Convert AU to game units for rendering
|
query
|
||||||
let scaled_position = position.0.0 * AU_TO_GAME_UNITS;
|
.get(target)
|
||||||
println!("scaled_position: {:?}", scaled_position);
|
.map_or(DVec3::ZERO, |(_, position, _)| position.0.0)
|
||||||
match transform {
|
});
|
||||||
Some(mut t) => {
|
for (_, position, mut transform) in query.iter_mut() {
|
||||||
// Update existing transform
|
transform.translation = ((position.0.0 - offset) * AU_TO_GAME_UNITS).as_vec3();
|
||||||
t.translation = scaled_position.as_vec3();
|
|
||||||
}
|
|
||||||
None => {
|
|
||||||
// Insert a new Transform if it doesn't exist
|
|
||||||
commands
|
|
||||||
.entity(entity)
|
|
||||||
.insert(Transform::from_translation(scaled_position.as_vec3()));
|
|
||||||
}
|
|
||||||
};
|
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
@ -149,32 +136,26 @@ fn setup_rendering(mut commands: Commands) {
|
|||||||
// Spawn camera with pan/orbit/zoom controls
|
// Spawn camera with pan/orbit/zoom controls
|
||||||
// Place it at a good distance to view the solar system
|
// Place it at a good distance to view the solar system
|
||||||
commands.spawn((
|
commands.spawn((
|
||||||
Camera3d::default(),
|
PanOrbitCamera {
|
||||||
|
zoom_lower_limit: 1e-6,
|
||||||
|
..default()
|
||||||
|
},
|
||||||
Camera {
|
Camera {
|
||||||
hdr: true,
|
hdr: true,
|
||||||
clear_color: ClearColorConfig::Custom(Color::BLACK),
|
clear_color: ClearColorConfig::Custom(Color::BLACK),
|
||||||
..default()
|
..default()
|
||||||
},
|
},
|
||||||
Projection::Perspective(PerspectiveProjection {
|
Projection::Perspective(PerspectiveProjection {
|
||||||
near: 1e-9, // Very close near plane for extreme zooming
|
near: 1e-8, // Very close near plane for extreme zooming
|
||||||
|
far: 1e-2,
|
||||||
..default()
|
..default()
|
||||||
}),
|
}),
|
||||||
Tonemapping::TonyMcMapface,
|
Tonemapping::TonyMcMapface,
|
||||||
Transform::from_translation(Vec3::new(0., 0., 10.0)),
|
Transform::from_translation(Vec3::new(0., 0., 10.0)),
|
||||||
Bloom::NATURAL,
|
Bloom::NATURAL,
|
||||||
PanOrbitCamera {
|
|
||||||
pan_sensitivity: 0.0, // Disable panning by setting sensitivity to 0
|
|
||||||
focus: Vec3::ZERO,
|
|
||||||
zoom_lower_limit: 1e-8,
|
|
||||||
..default()
|
|
||||||
},
|
|
||||||
));
|
));
|
||||||
|
|
||||||
commands.spawn(PointLight {
|
commands.spawn(PerfUiAllEntries::default());
|
||||||
color: Color::WHITE,
|
|
||||||
shadows_enabled: true,
|
|
||||||
..default()
|
|
||||||
});
|
|
||||||
}
|
}
|
||||||
|
|
||||||
fn setup_ui(mut commands: Commands) {
|
fn setup_ui(mut commands: Commands) {
|
||||||
@ -199,7 +180,7 @@ fn sync_name_labels(
|
|||||||
.any(|label| label.target_entity == entity);
|
.any(|label| label.target_entity == entity);
|
||||||
|
|
||||||
if !has_label {
|
if !has_label {
|
||||||
// Create new label
|
// Create new label with scaled font size
|
||||||
commands.spawn((
|
commands.spawn((
|
||||||
Text::new(name.0.0.clone()),
|
Text::new(name.0.0.clone()),
|
||||||
TextColor(Color::WHITE),
|
TextColor(Color::WHITE),
|
||||||
@ -218,40 +199,115 @@ fn sync_name_labels(
|
|||||||
ObjectLabel {
|
ObjectLabel {
|
||||||
target_entity: entity,
|
target_entity: entity,
|
||||||
},
|
},
|
||||||
|
LabelVisible(true), // Start visible by default
|
||||||
));
|
));
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
fn update_label_positions(
|
fn manage_label_overlaps(
|
||||||
mut label_query: Query<(&mut Node, &ObjectLabel, &mut Text), With<ObjectLabel>>,
|
mut label_query: Query<(&ObjectLabel, &mut LabelVisible)>,
|
||||||
objects_query: Query<(&Position, &Name, &Radius)>,
|
objects_query: Query<(&GlobalTransform, &Name, &Radius)>,
|
||||||
camera_query: Query<(&Camera, &GlobalTransform)>,
|
camera_query: Query<(&Camera, &GlobalTransform)>,
|
||||||
) {
|
) {
|
||||||
let Ok((camera, camera_transform)) = camera_query.single() else {
|
let Ok((camera, camera_transform)) = camera_query.single() else {
|
||||||
return;
|
return;
|
||||||
};
|
};
|
||||||
|
|
||||||
for (mut node, label, mut text) in label_query.iter_mut() {
|
// Collect all on-screen objects with their screen positions and radii
|
||||||
if let Ok((position, name, _radius)) = objects_query.get(label.target_entity) {
|
let mut visible_objects: Vec<(Entity, Vec2, f64, String)> = Vec::new();
|
||||||
let world_pos = position.0.0 * AU_TO_GAME_UNITS;
|
|
||||||
|
for (label, _) in label_query.iter() {
|
||||||
|
if let Ok((global_transform, name, radius)) = objects_query.get(label.target_entity) {
|
||||||
|
let world_pos = global_transform.translation();
|
||||||
|
if let Ok(screen_pos) = camera.world_to_viewport(camera_transform, world_pos) {
|
||||||
|
visible_objects.push((
|
||||||
|
label.target_entity,
|
||||||
|
screen_pos,
|
||||||
|
radius.0.0, // radius in AU
|
||||||
|
name.0.0.clone(),
|
||||||
|
));
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
// Reset all labels to visible first
|
||||||
|
for (_, mut visible) in label_query.iter_mut() {
|
||||||
|
visible.0 = true;
|
||||||
|
}
|
||||||
|
|
||||||
|
// Check for overlaps and hide smaller objects
|
||||||
|
const OVERLAP_THRESHOLD: f32 = 50.0; // pixels
|
||||||
|
|
||||||
|
for i in 0..visible_objects.len() {
|
||||||
|
for j in (i + 1)..visible_objects.len() {
|
||||||
|
let (entity_a, pos_a, radius_a, name_a) = &visible_objects[i];
|
||||||
|
let (entity_b, pos_b, radius_b, name_b) = &visible_objects[j];
|
||||||
|
|
||||||
|
let distance = pos_a.distance(*pos_b);
|
||||||
|
if distance < OVERLAP_THRESHOLD {
|
||||||
|
// Determine which label to hide based on radius (larger wins)
|
||||||
|
let entity_to_hide = if radius_a > radius_b {
|
||||||
|
*entity_b
|
||||||
|
} else if radius_b > radius_a {
|
||||||
|
*entity_a
|
||||||
|
} else {
|
||||||
|
// If radii are equal, prefer alphabetically first name
|
||||||
|
if name_a < name_b {
|
||||||
|
*entity_b
|
||||||
|
} else {
|
||||||
|
*entity_a
|
||||||
|
}
|
||||||
|
};
|
||||||
|
|
||||||
|
// Hide the smaller object's label
|
||||||
|
for (label, mut visible) in label_query.iter_mut() {
|
||||||
|
if label.target_entity == entity_to_hide {
|
||||||
|
visible.0 = false;
|
||||||
|
break;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
fn update_label_positions(
|
||||||
|
mut label_query: Query<(&mut Node, &ObjectLabel, &mut Text, &LabelVisible), With<ObjectLabel>>,
|
||||||
|
objects_query: Query<(&GlobalTransform, &Name, &Radius)>,
|
||||||
|
camera_query: Query<(&Camera, &GlobalTransform)>,
|
||||||
|
) {
|
||||||
|
let Ok((camera, camera_transform)) = camera_query.single() else {
|
||||||
|
return;
|
||||||
|
};
|
||||||
|
|
||||||
|
for (mut node, label, mut text, visible) in label_query.iter_mut() {
|
||||||
|
if !visible.0 {
|
||||||
|
// Label is marked as invisible due to overlap, hide it
|
||||||
|
node.display = Display::None;
|
||||||
|
continue;
|
||||||
|
}
|
||||||
|
|
||||||
|
if let Ok((global_transform, name, _radius)) = objects_query.get(label.target_entity) {
|
||||||
|
let world_pos = global_transform.translation();
|
||||||
|
if let Ok(screen_pos) = camera.world_to_viewport(camera_transform, world_pos) {
|
||||||
|
// Apply scale factor to label offset to maintain relative positioning
|
||||||
|
let scaled_offset = 10.0;
|
||||||
|
|
||||||
if let Ok(screen_pos) = camera.world_to_viewport(camera_transform, world_pos.as_vec3())
|
|
||||||
{
|
|
||||||
// Position the label on screen, offset slightly to avoid overlapping the object
|
// Position the label on screen, offset slightly to avoid overlapping the object
|
||||||
node.left = Val::Px(screen_pos.x + 10.0);
|
node.left = Val::Px(screen_pos.x + scaled_offset);
|
||||||
node.top = Val::Px(screen_pos.y - 10.0);
|
node.top = Val::Px(screen_pos.y - scaled_offset);
|
||||||
|
node.display = Display::Flex; // Make sure it's visible
|
||||||
|
|
||||||
// Update text in case name changed
|
// Update text in case name changed
|
||||||
text.0 = name.0.0.clone();
|
text.0 = name.0.0.clone();
|
||||||
} else {
|
} else {
|
||||||
// Object is off-screen, hide label by moving it off-screen
|
// Object is off-screen, hide label
|
||||||
node.left = Val::Px(-1000.0);
|
node.display = Display::None;
|
||||||
node.top = Val::Px(-1000.0);
|
|
||||||
}
|
}
|
||||||
} else {
|
} else {
|
||||||
// Target entity no longer exists, remove label
|
// Target entity no longer exists, hide label
|
||||||
// Note: In a more complex system, you might want to handle this in a separate cleanup system
|
node.display = Display::None;
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
@ -261,151 +317,245 @@ fn handle_label_clicks(
|
|||||||
(&Interaction, &ObjectLabel),
|
(&Interaction, &ObjectLabel),
|
||||||
(Changed<Interaction>, With<ObjectLabel>),
|
(Changed<Interaction>, With<ObjectLabel>),
|
||||||
>,
|
>,
|
||||||
trackable_objects: Query<(&Position, &Trackable, &Radius)>,
|
trackable_objects: Query<(&Transform, &Trackable, &Radius)>,
|
||||||
mut camera_query: Query<&mut PanOrbitCamera>,
|
mut camera: Single<&mut PanOrbitCamera>,
|
||||||
|
mut origin: ResMut<Origin>,
|
||||||
) {
|
) {
|
||||||
for (interaction, label) in interaction_query.iter() {
|
for (interaction, label) in interaction_query.iter() {
|
||||||
if *interaction == Interaction::Pressed {
|
if *interaction == Interaction::Pressed {
|
||||||
if let Ok((position, _trackable, radius)) = trackable_objects.get(label.target_entity) {
|
if let Ok((_target_transform, _trackable, radius)) =
|
||||||
if let Ok(mut pan_orbit) = camera_query.single_mut() {
|
trackable_objects.get(label.target_entity)
|
||||||
// Focus camera on the clicked object using target values for smooth transitions
|
{
|
||||||
pan_orbit.target_focus = (position.0.0 * AU_TO_GAME_UNITS).as_vec3();
|
// Calculate appropriate distance based on entity radius (with some padding)
|
||||||
pan_orbit.target_radius = (radius.0.0 * AU_TO_GAME_UNITS) as f32 * 4.;
|
let entity_radius = (radius.0.0 * AU_TO_GAME_UNITS) as f32;
|
||||||
|
camera.target_radius = entity_radius * 10.;
|
||||||
// Also set the immediate values to ensure it takes effect
|
camera.zoom_lower_limit = entity_radius * 4.;
|
||||||
// pan_orbit.focus = position.0.0.as_vec3();
|
camera.target_focus = Vec3::ZERO;
|
||||||
// pan_orbit.radius = Some(trackable.zoom_distance);
|
origin.target = Some(label.target_entity);
|
||||||
}
|
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
fn setup_solar_system(mut commands: Commands) {
|
fn handle_speed_controls(
|
||||||
// Sun - From NASA JPL Horizons data (J2000.0 epoch)
|
keyboard_input: Res<ButtonInput<KeyCode>>,
|
||||||
// Physical properties: Mass = 1988410 x 10^24 kg, Radius = 695700 km = 0.00465 AU
|
mut time: ResMut<Time<Virtual>>,
|
||||||
commands.spawn((
|
) {
|
||||||
ObjectBundle {
|
// Pause/Unpause with SPACE
|
||||||
name: Name(ObjectName("Sun".to_string())),
|
if keyboard_input.just_pressed(KeyCode::Space) {
|
||||||
position: Position(PositionAu(DVec3::new(0.0, 0.0, 0.0))), // At barycenter
|
if time.is_paused() {
|
||||||
velocity: Velocity(VelocityAuPerDay(DVec3::new(0.0, 0.0, 0.0))), // Stationary relative to barycenter
|
time.unpause();
|
||||||
mass: Mass(MassKg(1.988410e30)), // Solar mass in kg
|
println!("Simulation RESUMED (Speed: {}x)", time.relative_speed());
|
||||||
radius: Radius(DistanceAu(0.00465)), // Solar radius in AU (695700 km / 149597870.691)
|
} else {
|
||||||
},
|
time.pause();
|
||||||
Star,
|
println!("Simulation PAUSED");
|
||||||
Trackable {},
|
}
|
||||||
));
|
}
|
||||||
|
|
||||||
// Earth - From NASA JPL Horizons data (A.D. 2000-Jan-01 12:00:00.0000 TDB)
|
// Speed up with + or = key (double current speed, max 32x)
|
||||||
// Position and velocity vectors in ecliptic J2000.0 frame relative to Sun
|
if keyboard_input.just_pressed(KeyCode::Equal)
|
||||||
// Mass = 5.97219 x 10^24 kg, Mean radius = 6371.01 km = 0.0000426 AU
|
|| keyboard_input.just_pressed(KeyCode::NumpadAdd)
|
||||||
commands.spawn((
|
{
|
||||||
ObjectBundle {
|
if !time.is_paused() {
|
||||||
name: Name(ObjectName("Earth".to_string())),
|
let current_speed = time.relative_speed();
|
||||||
position: Position(PositionAu(DVec3::new(
|
let new_speed = (current_speed * 2.0).min(32.0);
|
||||||
-1.771350992727098e-1, // X = -0.177135 AU
|
time.set_relative_speed(new_speed);
|
||||||
9.672416867665306e-1, // Y = 0.967242 AU
|
println!("Speed: {}x", new_speed);
|
||||||
-4.085281582511366e-6, // Z = -4.085e-6 AU
|
}
|
||||||
))),
|
}
|
||||||
velocity: Velocity(VelocityAuPerDay(DVec3::new(
|
|
||||||
-1.720762506872895e-2, // VX = -0.0172076 AU/day
|
|
||||||
-3.158782144324866e-3, // VY = -0.00315878 AU/day
|
|
||||||
1.049888594613343e-7, // VZ = 1.04989e-7 AU/day
|
|
||||||
))),
|
|
||||||
mass: Mass(MassKg(5.97219e24)), // Earth mass in kg
|
|
||||||
radius: Radius(DistanceAu(0.0000426)), // Mean radius in AU (6371.01 km / 149597870.691)
|
|
||||||
},
|
|
||||||
Trackable {},
|
|
||||||
));
|
|
||||||
|
|
||||||
// Moon - From NASA JPL Horizons data (A.D. 2000-Jan-01 12:00:00.0000 TDB)
|
// Speed down with - key (halve current speed, min 1.0x)
|
||||||
// Position and velocity vectors in ecliptic J2000.0 frame relative to Sun
|
if keyboard_input.just_pressed(KeyCode::Minus)
|
||||||
// Mass = 7.349 x 10^22 kg, Mean radius = 1737.53 km = 0.0000116 AU
|
|| keyboard_input.just_pressed(KeyCode::NumpadSubtract)
|
||||||
commands.spawn((
|
{
|
||||||
ObjectBundle {
|
if !time.is_paused() {
|
||||||
name: Name(ObjectName("Moon".to_string())),
|
let current_speed = time.relative_speed();
|
||||||
position: Position(PositionAu(DVec3::new(
|
let new_speed = (current_speed * 0.5).max(1.0);
|
||||||
-1.790843809223965e-1, // X = -0.179084 AU
|
time.set_relative_speed(new_speed);
|
||||||
9.654035607264573e-1, // Y = 0.965404 AU
|
println!("Speed: {}x", new_speed);
|
||||||
2.383726922995396e-4, // Z = 0.000238373 AU
|
}
|
||||||
))),
|
}
|
||||||
velocity: Velocity(VelocityAuPerDay(DVec3::new(
|
|
||||||
-1.683595459141215e-2, // VX = -0.0168360 AU/day
|
// Reset to normal speed with R
|
||||||
-3.580960720855671e-3, // VY = -0.00358096 AU/day
|
if keyboard_input.just_pressed(KeyCode::KeyR) {
|
||||||
-6.540550604528720e-6, // VZ = -6.54055e-6 AU/day
|
time.set_relative_speed(1.0);
|
||||||
))),
|
time.unpause();
|
||||||
mass: Mass(MassKg(7.349e22)), // Moon mass in kg
|
println!("Speed reset to 1x");
|
||||||
radius: Radius(DistanceAu(0.0000116)), // Mean radius in AU (1737.53 km / 149597870.691)
|
}
|
||||||
},
|
}
|
||||||
Trackable {},
|
|
||||||
));
|
const AU_TO_KM: f64 = 149597870.691;
|
||||||
|
|
||||||
|
fn setup_solar_system(mut commands: Commands, asset_server: Res<AssetServer>) {
|
||||||
|
// Load initial state from RON file
|
||||||
|
let initial_state_content = match std::fs::read_to_string("assets/initial_state.ron") {
|
||||||
|
Ok(content) => content,
|
||||||
|
Err(err) => {
|
||||||
|
error!("Failed to read initial_state.ron: {}", err);
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
};
|
||||||
|
|
||||||
|
let initial_state: InitialState = match ron::from_str(&initial_state_content) {
|
||||||
|
Ok(state) => state,
|
||||||
|
Err(err) => {
|
||||||
|
error!("Failed to parse initial_state.ron: {}", err);
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
};
|
||||||
|
|
||||||
|
for body_data in initial_state.bodies {
|
||||||
|
// Convert radius from km to AU
|
||||||
|
let radius_au = body_data.radius / AU_TO_KM; // km to AU conversion
|
||||||
|
|
||||||
|
// Convert mass from kg to solar masses
|
||||||
|
let mass_solar = body_data.mass / SOLAR_MASS_KG;
|
||||||
|
|
||||||
|
// Create base bundle
|
||||||
|
let mut entity_commands = commands.spawn((
|
||||||
|
ObjectBundle {
|
||||||
|
name: Name(ObjectName(body_data.name.clone())),
|
||||||
|
position: Position(PositionAu(DVec3::new(
|
||||||
|
body_data.position.0,
|
||||||
|
body_data.position.1,
|
||||||
|
body_data.position.2,
|
||||||
|
))),
|
||||||
|
velocity: Velocity(VelocityAuPerDay(DVec3::new(
|
||||||
|
body_data.velocity.0,
|
||||||
|
body_data.velocity.1,
|
||||||
|
body_data.velocity.2,
|
||||||
|
))),
|
||||||
|
mass: Mass(MassSolarMass(mass_solar)),
|
||||||
|
radius: Radius(DistanceAu(radius_au)),
|
||||||
|
},
|
||||||
|
Trackable {},
|
||||||
|
Transform::default(),
|
||||||
|
Visibility::default(),
|
||||||
|
));
|
||||||
|
let scene_handle = asset_server.load(format!("models/{}#Scene0", body_data.model.path));
|
||||||
|
entity_commands.with_child((
|
||||||
|
SceneRoot(scene_handle.clone()),
|
||||||
|
Transform::from_scale(
|
||||||
|
Vec3::new(
|
||||||
|
body_data.model.scale.0,
|
||||||
|
body_data.model.scale.1,
|
||||||
|
body_data.model.scale.2,
|
||||||
|
) / AU_TO_KM as f32
|
||||||
|
* 10000.,
|
||||||
|
),
|
||||||
|
));
|
||||||
|
|
||||||
|
// Add special components for Sun and Earth
|
||||||
|
match body_data.name.as_str() {
|
||||||
|
"Sun" => {
|
||||||
|
entity_commands.insert(Star);
|
||||||
|
entity_commands.insert(NeedsEmissiveEnhancement);
|
||||||
|
entity_commands.insert(PointLight {
|
||||||
|
color: Color::WHITE,
|
||||||
|
shadows_enabled: true,
|
||||||
|
..default()
|
||||||
|
});
|
||||||
|
}
|
||||||
|
"Earth" => {
|
||||||
|
entity_commands.insert(Earth);
|
||||||
|
}
|
||||||
|
_ => {}
|
||||||
|
}
|
||||||
|
|
||||||
|
info!("Spawned celestial body: {}", body_data.name);
|
||||||
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
// High precision constants
|
// High precision constants
|
||||||
const G_SI: f64 = 6.67430e-11; // Gravitational constant in m³/kg/s² (2018 CODATA value)
|
const SOLAR_MASS_KG: f64 = 1.98841e30; // kg (for mass conversion)
|
||||||
const AU_TO_M: f64 = 149597870691.0; // AU to meters (IAU 2012 definition, exact)
|
|
||||||
const DAY_TO_S: f64 = 86400.0; // Day to seconds (exact)
|
|
||||||
|
|
||||||
// Pre-calculated G in AU³/kg/day² units for optimization
|
// Gaussian gravitational constant (standard in astronomy)
|
||||||
// G_AU = G_SI * (day²/s²) / (AU³/m³)
|
const K_GAUSS: f64 = 0.01720209895; // AU^(3/2) / (solar_mass^(1/2) × day)
|
||||||
// G_AU = G_SI * (DAY_TO_S²) / (AU_TO_M³)
|
|
||||||
const G_AU: f64 = G_SI * (DAY_TO_S * DAY_TO_S) / (AU_TO_M * AU_TO_M * AU_TO_M);
|
|
||||||
|
|
||||||
const STEPS: usize = 100;
|
// G in AU^3 / (solar_mass day^2)
|
||||||
// Time step calculation:
|
// Derived from Gaussian constant: G_AU = k² where k is the Gaussian constant
|
||||||
// FixedUpdate runs at 64fps, 1 game second = 7 days, 100 steps per FixedUpdate
|
// This gives G×M_sun in AU³/day² units, and since we use solar mass units (M_sun = 1), G_AU = k²
|
||||||
// DT = (7 days / 64 fps) / 100 steps = 7 / (64 * 100) = 0.00109375 days per step
|
const G_AU: f64 = K_GAUSS * K_GAUSS;
|
||||||
const DT: f64 = 7.0 / (64.0 * STEPS as f64); // Time step in days
|
|
||||||
|
|
||||||
|
const STEPS: usize = 20; // Number of steps per fixed update
|
||||||
|
// If FixedUpdate is 64 Hz and you want 1 day per game second: DT = 1/(64*STEPS) day/step
|
||||||
|
const DT: f64 = 1.0 / (64.0 * STEPS as f64);
|
||||||
fn n_body(mut query: Query<(&Mass, &mut Position, &mut Velocity)>) {
|
fn n_body(mut query: Query<(&Mass, &mut Position, &mut Velocity)>) {
|
||||||
// Collect all bodies data (mass, position, velocity)
|
// Pull data out once. This copy lets us integrate freely without borrow issues.
|
||||||
|
// (If you want zero copies, use a Resource scratch buffer and reuse it across frames.)
|
||||||
let mut bodies: Vec<(f64, DVec3, DVec3)> = query
|
let mut bodies: Vec<(f64, DVec3, DVec3)> = query
|
||||||
.iter()
|
.iter()
|
||||||
.map(|(mass, pos, vel)| (mass.0.0, pos.0.0, vel.0.0))
|
.map(|(mass, pos, vel)| (mass.0.0, pos.0.0, vel.0.0))
|
||||||
.collect();
|
.collect();
|
||||||
|
|
||||||
// Perform integration steps
|
let n = bodies.len();
|
||||||
for _ in 0..STEPS {
|
if n < 2 {
|
||||||
// Calculate forces for all bodies
|
// Nothing to do; write back if needed and return
|
||||||
let mut forces: Vec<DVec3> = vec![DVec3::ZERO; bodies.len()];
|
for (i, (_m, mut pos, mut vel)) in query.iter_mut().enumerate() {
|
||||||
|
if let Some(b) = bodies.get(i) {
|
||||||
|
pos.0.0 = b.1;
|
||||||
|
vel.0.0 = b.2;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
return;
|
||||||
|
}
|
||||||
|
|
||||||
for i in 0..bodies.len() {
|
// Single reusable acceleration buffer
|
||||||
for j in 0..bodies.len() {
|
let mut acc: Vec<DVec3> = vec![DVec3::ZERO; n];
|
||||||
if i != j {
|
|
||||||
let r_vec = bodies[j].1 - bodies[i].1; // Position difference in AU
|
|
||||||
let r_mag_au = r_vec.length();
|
|
||||||
|
|
||||||
if r_mag_au > 1e-10 {
|
// Pairwise acceleration accumulation (O(n^2)/2) with Newton's 3rd law
|
||||||
// Avoid division by zero
|
let compute_accelerations = |bodies: &[(f64, DVec3, DVec3)], acc: &mut [DVec3]| {
|
||||||
// Calculate force directly in AU/day² units
|
acc.fill(DVec3::ZERO);
|
||||||
let force_magnitude =
|
|
||||||
G_AU * bodies[i].0 * bodies[j].0 / (r_mag_au * r_mag_au);
|
|
||||||
let acceleration = force_magnitude / bodies[i].0; // F/m = a
|
|
||||||
let force_vec = r_vec.normalize() * acceleration;
|
|
||||||
|
|
||||||
forces[i] += force_vec;
|
for i in 0..n - 1 {
|
||||||
}
|
let (mi, pi, _) = bodies[i];
|
||||||
|
for j in (i + 1)..n {
|
||||||
|
let (mj, pj, _) = bodies[j];
|
||||||
|
|
||||||
|
let r = pj - pi; // AU
|
||||||
|
let r2 = r.length_squared(); // AU^2
|
||||||
|
// Tighter epsilon in AU^2; avoids division by ~0 without killing legit close passes
|
||||||
|
if r2 > 1e-20 {
|
||||||
|
// a_i = G * m_j * r / r^3, a_j = -G * m_i * r / r^3
|
||||||
|
let inv_r = r2.sqrt().recip(); // 1 / r
|
||||||
|
let inv_r3 = inv_r * inv_r * inv_r; // 1 / r^3
|
||||||
|
|
||||||
|
let a_i = r * (G_AU * mj * inv_r3);
|
||||||
|
let a_j = r * (G_AU * mi * inv_r3);
|
||||||
|
|
||||||
|
acc[i] += a_i;
|
||||||
|
acc[j] -= a_j; // opposite direction
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
};
|
||||||
|
|
||||||
// Update velocities and positions using Verlet integration
|
// Leapfrog / velocity-Verlet
|
||||||
for i in 0..bodies.len() {
|
for _ in 0..STEPS {
|
||||||
// Update velocity: v += a * dt
|
// v += a(q) * dt/2
|
||||||
bodies[i].2 += forces[i] * DT;
|
compute_accelerations(&bodies, &mut acc);
|
||||||
|
for i in 0..n {
|
||||||
|
bodies[i].2 += acc[i] * (DT * 0.5);
|
||||||
|
}
|
||||||
|
|
||||||
// Update position: x += v * dt
|
// q += v * dt
|
||||||
let velocity = bodies[i].2;
|
for i in 0..n {
|
||||||
bodies[i].1 += velocity * DT;
|
let vel = bodies[i].2; // copy DVec3 (cheap, it's just 3 f64s)
|
||||||
|
bodies[i].1 += vel * DT;
|
||||||
|
}
|
||||||
|
|
||||||
|
// v += a(q_new) * dt/2
|
||||||
|
compute_accelerations(&bodies, &mut acc);
|
||||||
|
for i in 0..n {
|
||||||
|
bodies[i].2 += acc[i] * (DT * 0.5);
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
// Write back updated positions and velocities
|
// Write back
|
||||||
for (i, (_mass, mut pos, mut vel)) in query.iter_mut().enumerate() {
|
for (i, (_mass, mut pos, mut vel)) in query.iter_mut().enumerate() {
|
||||||
if let Some(body) = bodies.get(i) {
|
let (_, p, v) = bodies[i];
|
||||||
pos.0.0 = body.1;
|
pos.0.0 = p;
|
||||||
vel.0.0 = body.2;
|
vel.0.0 = v;
|
||||||
}
|
|
||||||
}
|
}
|
||||||
}
|
}
|
||||||
|
|
||||||
@ -415,15 +565,26 @@ fn main() {
|
|||||||
primary_window: Some(Window {
|
primary_window: Some(Window {
|
||||||
title: "Solar Sim".to_string(),
|
title: "Solar Sim".to_string(),
|
||||||
mode: WindowMode::BorderlessFullscreen(MonitorSelection::Primary),
|
mode: WindowMode::BorderlessFullscreen(MonitorSelection::Primary),
|
||||||
|
resolution: WindowResolution::default().with_scale_factor_override(2.0),
|
||||||
..default()
|
..default()
|
||||||
}),
|
}),
|
||||||
..default()
|
..default()
|
||||||
}))
|
}))
|
||||||
.add_plugins(PanOrbitCameraPlugin)
|
|
||||||
.add_plugins(EguiPlugin::default())
|
.add_plugins(EguiPlugin::default())
|
||||||
|
.add_plugins(PanOrbitCameraPlugin)
|
||||||
|
.register_type::<Name>()
|
||||||
|
.register_type::<Radius>()
|
||||||
|
.register_type::<DistanceAu>()
|
||||||
|
.register_type::<Mass>()
|
||||||
|
.register_type::<MassSolarMass>()
|
||||||
.add_plugins(WorldInspectorPlugin::new())
|
.add_plugins(WorldInspectorPlugin::new())
|
||||||
.add_plugins(SolarRenderingPlugin)
|
.add_plugins(SolarRenderingPlugin) // we want Bevy to measure these values for us:
|
||||||
.add_systems(Startup, setup_solar_system)
|
.add_plugins(bevy::diagnostic::FrameTimeDiagnosticsPlugin::default())
|
||||||
.add_systems(FixedUpdate, n_body)
|
.add_plugins(bevy::diagnostic::EntityCountDiagnosticsPlugin)
|
||||||
|
.add_plugins(bevy::diagnostic::SystemInformationDiagnosticsPlugin)
|
||||||
|
.add_plugins(bevy::render::diagnostic::RenderDiagnosticsPlugin)
|
||||||
|
.add_plugins(PerfUiPlugin)
|
||||||
|
.add_systems(Startup, (setup_solar_system).chain())
|
||||||
|
.add_systems(FixedUpdate, n_body) // Use the optimized n-body system
|
||||||
.run();
|
.run();
|
||||||
}
|
}
|
||||||
|
|||||||
Loading…
Reference in New Issue
Block a user