Planetary theory used to compute the ephemeris
Planetary theory used to compute the ephemeris
SkyBoT - Coordinates of the resolved target
Reference system (EQJ2000|ECJ2000)
Solar system object number
Solar system object name
Astrometric J2000 right ascension
Astrometric J2000 declination
Object classification
Visual magnitude
Uncertainty on the (RA,DEC) coordinates
Motion in right ascension d(RA)cos(DEC)
Motion in declination d(DEC)
Distance from observer
Distance from the Sun
Phase angle, e.g. elongation of earth from sun as seen from object
Solar elongation, e.g. elongation of object from sun as seen from Earth
Mean J2000 heliocentric position vector, x component
Mean J2000 heliocentric position vector, y component
Mean J2000 heliocentric position vector, z component
Mean J2000 heliocentric velocity vector, x component
Mean J2000 heliocentric velocity vector, y component
Mean J2000 heliocentric velocity vector, z component
Reference epoch of the position/velocity vector
External link to hint the target
85
Io
05 47 44.0494
+06 54 18.017
MB>Middle
12.5
0.246
-25.6063
5.361
2.036683865
2.919068883
10.20
148.30
-0.249713156
2.837462778
0.604532868
-0.009511038
0.000932702
-0.000600503
2453380
http://vizier.u-strasbg.fr/cgi-bin/VizieR-5?-source=B/astorb/astorb&Name===Io
501
Io
13 09 24.0088
-05 54 21.605
Satellite
6.0
0.010
-8.5944
0.000
5.259884412
5.451731277
10.34
96.03
-4.9939146185637
-1.5602167889683
-0.5412248853264
0.0142143192929
0.0087206268482
0.0041296667215
2453384.92154000001
https://api.ssodnet.imcce.fr/quaero/1/sso?q=Io AND type:Satellite