1862 Apollo help
Last update: 2026-04-01 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
3.087E-10
Unit
Eccentricity (e)
Value
0.560180
1-sigma variation
7.591E-9
Unit
-
Inclination (i)
Value
6.3522
1-sigma variation
2.275E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5030
1-sigma variation
1.167E-5
Unit
Arg. of Perihelion (ω)
Value
286.0977
1-sigma variation
1.218E-5
Unit
Mean Anomaly (M)
Value
224.36160
1-sigma variation
2.120E-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
-3.76397
1-sigma variation
0.28304
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.52838E-20-5.96207E-19-1.40348E-16-3.07058E-153.21079E-15-5.49697E-164.36791E-11
e-5.96207E-195.76179E-17-9.46251E-162.13647E-14-3.29230E-148.48691E-151.19156E-9
i-1.40348E-16-9.46251E-165.17500E-126.90021E-12-6.38597E-12-7.77020E-131.29592E-7
Ω-3.07058E-152.13647E-146.90021E-121.36118E-10-1.41094E-102.09684E-11-8.05048E-7
ω3.21079E-15-3.29230E-14-6.38597E-12-1.41094E-101.48472E-10-2.29311E-115.94575E-7
M-5.49697E-168.48691E-15-7.77020E-132.09684E-11-2.29311E-114.49338E-12-1.32000E-7
A24.36791E-111.19156E-91.29592E-7-8.05048E-75.94575E-7-1.32000E-78.01126E-2
Date of computation: 2026-04-01 13:00 UTC
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