solar-sim/assets/earth.txt
2025-08-13 20:13:35 +09:00

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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
*******************************************************************************
Revised: April 12,
2021 Earth 399
GEOPHYSICAL PROPERTIES (revised May 9,
2022):
Vol. Mean Radius (km) = 6371.01+-0.02 Mass x10^24 (kg)= 5.97219+-0.0006
Equ. radius, km = 6378.137 Mass layers:
Polar axis, km = 6356.752 Atmos = 5.1 x 10^18 kg
Flattening = 1/298.257223563 oceans = 1.4 x 10^21 kg
Density, g/cm^3 = 5.51 crust = 2.6 x 10^22 kg
J2 (IERS 2010) = 0.00108262545 mantle = 4.043 x 10^24 kg
g_p, m/s^2 (polar) = 9.8321863685 outer core = 1.835 x 10^24 kg
g_e, m/s^2 (equatorial) = 9.7803267715 inner core = 9.675 x 10^22 kg
g_o, m/s^2 = 9.82022 Fluid core rad = 3480 km
GM, km^3/s^2 = 398600.435436 Inner core rad = 1215 km
GM 1-sigma, km^3/s^2 = 0.0014 Escape velocity = 11.186 km/s
Rot. Rate (rad/s) = 0.00007292115 Surface area:
Mean sidereal day, hr = 23.9344695944 land = 1.48 x 10^8 km
Mean solar day 2000.0, s = 86400.002 sea = 3.62 x 10^8 km
Mean solar day 1820.0, s = 86400.0 Love no., k2 = 0.299
Moment of inertia = 0.3308 Atm. pressure = 1.0 bar
Mean surface temp (Ts), K= 287.6 Volume, km^3 = 1.08321 x 10^12
Mean effect. temp (Te), K= 255 Magnetic moment = 0.61 gauss Rp^3
Geometric albedo = 0.367 Vis. mag. V(1,
0)= -3.86
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
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
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Ephemeris / API_USER Wed Aug 13 04: 00: 37 2025 Pasadena, USA / Horizons
*******************************************************************************
Target body name: Earth (399) {source: DE441
}
Center body name: Sun (10) {source: DE441
}
Center-site name: BODY CENTER
*******************************************************************************
Start time : A.D. 2000-Jan-01 12: 00: 00.0000 TDB
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 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
*******************************************************************************
$$SOE
2451545.000000000 = A.D. 2000-Jan-01 12: 00: 00.0000 TDB
X =-1.771350992727098E-01 Y = 9.672416867665306E-01 Z =-4.085281582511366E-06
VX=-1.720762506872895E-02 VY=-3.158782144324866E-03 VZ= 1.049888594613343E-07
2451545.000694444 = A.D. 2000-Jan-01 12: 01: 00.0000 TDB
X =-1.771470489993106E-01 Y = 9.672394930949845E-01 Z =-4.085208640488331E-06
VX=-1.720758754114626E-02 VY=-3.158991907845201E-03 VZ= 1.050842029536420E-07
$$EOE
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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
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