Files
astronomy/generate/lagrange/check_moon.txt

116 lines
5.9 KiB
Plaintext

*******************************************************************************
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
Radius (gravity), km = 1738.0 Surface emissivity = 0.92
Radius (IAU), km = 1737.4 GM, km^3/s^2 = 4902.800066
Density, g/cm^3 = 3.3437 GM 1-sigma, km^3/s^2 = +-0.0001
V(1,0) = +0.21 Surface accel., m/s^2 = 1.62
Earth/Moon mass ratio = 81.3005690769 Farside crust. thick. = ~80 - 90 km
Mean crustal density = 2.97+-.07 g/cm^3 Nearside crust. thick.= 58+-8 km
Heat flow, Apollo 15 = 3.1+-.6 mW/m^2 Mean angular diameter = 31'05.2"
Heat flow, Apollo 17 = 2.2+-.5 mW/m^2 Sid. rot. rate, rad/s = 0.0000026617
Geometric Albedo = 0.12 Mean solar day = 29.5306 d
Obliquity to orbit = 6.67 deg Orbit period = 27.321582 d
Semi-major axis, a = 384400 km Eccentricity = 0.05490
Mean motion, rad/s = 2.6616995x10^-6 Inclination = 5.145 deg
Apsidal period = 3231.50 d Nodal period = 6798.38 d
Perihelion Aphelion Mean
Solar Constant (W/m^2) 1414+-7 1323+-7 1368+-7
Maximum Planetary IR (W/m^2) 1314 1226 1268
Minimum Planetary IR (W/m^2) 5.2 5.2 5.2
********************************************************************************
*******************************************************************************
Ephemeris / WWW_USER Thu Feb 17 18:30:56 2022 Pasadena, USA / Horizons
*******************************************************************************
Target body name: Moon (301) {source: DE441}
Center body name: Earth (399) {source: DE441}
Center-site name: BODY CENTER
*******************************************************************************
Start time : A.D. 2020-Mar-24 06:00:00.0000 TDB
Stop time : A.D. 2020-Mar-25 06:00:00.0000 TDB
Step-size : 1440 minutes
*******************************************************************************
Center geodetic : 0.00000000,0.00000000,0.0000000 {E-lon(deg),Lat(deg),Alt(km)}
Center cylindric: 0.00000000,0.00000000,0.0000000 {E-lon(deg),Dxy(km),Dz(km)}
Center radii : 6378.1 x 6378.1 x 6356.8 km {Equator, meridian, pole}
Output units : AU-D
Output type : GEOMETRIC cartesian states
Output format : 2 (position and velocity)
EOP file : eop.220216.p220512
EOP coverage : DATA-BASED 1962-JAN-20 TO 2022-FEB-16. PREDICTS-> 2022-MAY-11
Reference frame : ICRF
*******************************************************************************
JDTDB
X Y Z
VX VY VZ
*******************************************************************************
$$SOE
2458932.750000000 = A.D. 2020-Mar-24 06:00:00.0000 TDB
X = 2.705953999132032E-03 Y = 1.893525408300819E-04 Z =-1.752774223513111E-04
VX=-1.991849279045934E-05 VY= 5.148133848757774E-04 VZ= 2.218646176831359E-04
2458933.750000000 = A.D. 2020-Mar-25 06:00:00.0000 TDB
X = 2.626621595899715E-03 Y = 6.961333356580973E-04 Z = 4.889489555029374E-05
VX=-1.381661604524936E-04 VY= 4.949404874160148E-04 VZ= 2.247966555360729E-04
$$EOE
*******************************************************************************
TIME
Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
continuous relativistic coordinate time is equivalent to the relativistic
proper time of a clock at rest in a reference frame comoving 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 dates prior to 1582-Oct-15 are in the Julian calendar system.
Later calendar dates are in the Gregorian system.
REFERENCE FRAME AND COORDINATES
International Celestial Reference Frame (ICRF)
The ICRF is an adopted reference frame whose axes are defined relative to
fixed extragalactic radio sources distributed across the sky.
The ICRF was aligned with the prior FK5/J2000 dynamical system at the ~0.02
arcsecond level but is not identical and has no associated standard 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/hrzn_batch.txt
scripts https://ssd.jpl.nasa.gov/ftp/ssd/SCRIPTS
Author : Jon.D.Giorgini@jpl.nasa.gov
*******************************************************************************