1862 Apollo help
Last update: 2026-08-31 13:00 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
61200.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.470715
1-sigma variation
3.085E-10
Unit
Eccentricity (e)
Value
0.560180
1-sigma variation
7.578E-9
Unit
-
Inclination (i)
Value
6.3522
1-sigma variation
2.255E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5030
1-sigma variation
1.165E-5
Unit
Arg. of Perihelion (ω)
Value
286.0977
1-sigma variation
1.217E-5
Unit
Mean Anomaly (M)
Value
224.36160
1-sigma variation
2.119E-6
Unit
Perihelion distance
Value
0.646850
1-sigma variation
Unit
Aphelion distance
Value
2.294580
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.120642
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.189278
1-sigma variation
Unit
MOID
Value
0.026318
1-sigma variation
Unit
Orbit Period
Value
651.4653
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
A2
Value
-3.77131
1-sigma variation
0.28268
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.51575E-20-5.97558E-19-1.37108E-16-3.06461E-153.20528E-15-5.49978E-164.37184E-11
e-5.97558E-195.74253E-17-9.28980E-162.14294E-14-3.29483E-148.47577E-151.18620E-9
i-1.37108E-16-9.28980E-165.08606E-126.74473E-12-6.23919E-12-7.69434E-131.27852E-7
Ω-3.06461E-152.14294E-146.74473E-121.35835E-10-1.40833E-102.09825E-11-8.06984E-7
ω3.20528E-15-3.29483E-14-6.23919E-12-1.40833E-101.48225E-10-2.29424E-115.97476E-7
M-5.49978E-168.47577E-15-7.69434E-132.09825E-11-2.29424E-114.49206E-12-1.32130E-7
A24.37184E-111.18620E-91.27852E-7-8.06984E-75.97476E-7-1.32130E-77.99060E-2
Date of computation: 2026-08-31 13:00 UTC
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