1862 Apollo help
Last update: 2024-05-20 14:31 UTC
Epoch
Orbit properties
  • Epoch
  • Semimajor Axis
  • Eccentricity (e)
  • Inclination (i)
  • Long. of Ascending Node (Ω)
  • Arg. of Perihelion (ω)
  • Mean Anomaly (M)
  • Perihelion distance
  • Aphelion distance
  • Asc. Node-Earth Sep.
  • Desc. Node-Earth Sep.
  • MOID
  • Orbit Period
  • U parameter
Value
1-sigma variation
Unit
Epoch
Value
60400.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.470569
1-sigma variation
2.941E-10
Unit
Eccentricity (e)
Value
0.559902
1-sigma variation
7.452E-9
Unit
-
Inclination (i)
Value
6.3525
1-sigma variation
2.370E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5560
1-sigma variation
1.142E-5
Unit
Arg. of Perihelion (ω)
Value
286.0393
1-sigma variation
1.194E-5
Unit
Mean Anomaly (M)
Value
142.31869
1-sigma variation
1.976E-6
Unit
Perihelion distance
Value
0.647195
1-sigma variation
Unit
Aphelion distance
Value
2.293943
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.118458
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.188393
1-sigma variation
Unit
MOID
Value
0.025860
1-sigma variation
Unit
Orbit Period
Value
651.3679
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
A2
Value
-3.70423
1-sigma variation
0.27892
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a8.64860E-20-7.55147E-19-1.55388E-16-2.90797E-153.07681E-15-4.85179E-163.31280E-11
e-7.55147E-195.55374E-17-1.10986E-152.09007E-14-3.20812E-148.02001E-151.13608E-9
i-1.55388E-16-1.10986E-155.61527E-127.24775E-12-6.66460E-12-9.64022E-131.41259E-7
Ω-2.90797E-152.09007E-147.24775E-121.30489E-10-1.35308E-101.86304E-11-7.33844E-7
ω3.07681E-15-3.20812E-14-6.66460E-12-1.35308E-101.42465E-10-2.04977E-115.34324E-7
M-4.85179E-168.02001E-15-9.64022E-131.86304E-11-2.04977E-113.90438E-12-1.10373E-7
A23.31280E-111.13608E-91.41259E-7-7.33844E-75.34324E-7-1.10373E-77.77962E-2
Date of computation: 2024-04-23 10:08 UTC
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