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OpenSpace/tests/horizonsTest/timerange_no_time.hrz
2022-05-24 09:34:25 +02:00

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Revised: Apr 21, 2022 Gaia Observatory -139479
http://sci.esa.int/gaia/
BACKGROUND:
Gaia is designed and operated by the European Space Agency. It launched
December 19, 2013 @ 09:12 UTC on a Soyuz launcher from Kourou, French Guiana.
On 2014-Jan-08, it arrived at its operational Lissajous orbit around the
gravitationally stable Earth-Sun Lagrange-point L2, roughly 1.5 million km
from Earth in the direction opposite the Sun. The orbit is not shadowed by
Earth eclipses. The orbit period is about 180 days; the size of the orbit
is typically 340,000 x 90,000 km.
MISSION:
Gaia's 5-year primary mission is to ...
* Measure the positions of ~1 billion stars both in our Galaxy and other
members of the Local Group, with an accuracy down to 24 uas
* Perform spectral and photometric measurements of all objects
* Derive space velocities of the Galaxy's constituent stars using the
stellar distances and motions
* Create a three-dimensional structural map of the Galaxy
Additional expected results include extrasolar planet detection, brown dwarf
detection, solar system asteroid discoveries, supernova early detection, and
testing of Einstein's general relativity.
GAIA SPACECRAFT:
Spacecraft dry mass total 1392 kg
Propellant 237 kg
Total launch mass 2029 kg
Power: 12.8 m^2 solar array provides up to 1910 Watts
SCIENCE INSTRUMENTS:
Single integrated instrument that comprises three major functions:
astrometry, photometry (320-1000 nm) and spectrometry (846-874 nm).
The three functions use two common telescopes and a shared focal plane,
with each function having a dedicated area on the large 0.5m x 1m CCD
detector array.
SPACECRAFT TRAJECTORY (from ESA 2022-Apr-19, predicts thereafter)
Trajectory name Start Stop
-------------------------------------------- ----------- -----------
ORB1_20220419_000001 2013-Dec-19 2026-Sep-14
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Ephemeris / API_USER Mon May 23 05:28:00 2022 Pasadena, USA / Horizons
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Target body name: Gaia (spacecraft) (-139479) {source: gaia_merged}
Center body name: Earth-Moon Barycenter (3) {source: gaia_merged}
Center-site name: BODY CENTER
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Start time : A.D. 2022-May-22 00:00:00.0000 TDB
Stop time : A.D. 2022-May-23 00:00:00.0000 TDB
Step-size : 720 minutes
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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 : (undefined)
Output units : KM-S
Output type : GEOMETRIC cartesian states
Output format : 1 (position only)
Reference frame : Ecliptic of J2000.0
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JDTDB
X Y Z
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$$SOE
2459721.500000000 = A.D. 2022-May-22 00:00:00.0000 TDB
-1.005869741260714E+06 -1.229636409807553E+06 5.553741267973231E+04
2459722.000000000 = A.D. 2022-May-22 12:00:00.0000 TDB
-9.976647219177654E+05 -1.235095646685846E+06 5.296169462755765E+04
2459722.500000000 = A.D. 2022-May-23 00:00:00.0000 TDB
-9.893621107980320E+05 -1.240524898186224E+06 5.037219698871591E+04
$$EOE
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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
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:
JDTDB Julian Day Number, Barycentric Dynamical Time
X X-component of position vector (km)
Y Y-component of position vector (km)
Z Z-component of position vector (km)
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
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