1862 Apollo help
Last update: 2025-12-28 13:16 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
61000.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.470924
1-sigma variation
3.057E-10
Unit
Eccentricity (e)
Value
0.559918
1-sigma variation
7.642E-9
Unit
-
Inclination (i)
Value
6.3514
1-sigma variation
2.358E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5416
1-sigma variation
1.172E-5
Unit
Arg. of Perihelion (ω)
Value
286.0509
1-sigma variation
1.223E-5
Unit
Mean Anomaly (M)
Value
113.88454
1-sigma variation
2.093E-6
Unit
Perihelion distance
Value
0.647327
1-sigma variation
Unit
Aphelion distance
Value
2.294520
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.119240
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.187300
1-sigma variation
Unit
MOID
Value
0.026011
1-sigma variation
Unit
Orbit Period
Value
651.6039
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
A2
Value
-3.74979
1-sigma variation
0.28451
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.34374E-20-6.06299E-19-1.63866E-16-3.05308E-153.19343E-15-5.28402E-164.18410E-11
e-6.06299E-195.83988E-17-1.01002E-152.10985E-14-3.28227E-148.48275E-151.21370E-9
i-1.63866E-16-1.01002E-155.55843E-127.57401E-12-7.02016E-12-8.31140E-131.36996E-7
Ω-3.05308E-152.10985E-147.57401E-121.37305E-10-1.42189E-102.05549E-11-7.96186E-7
ω3.19343E-15-3.28227E-14-7.02016E-12-1.42189E-101.49514E-10-2.25191E-115.81812E-7
M-5.28402E-168.48275E-15-8.31140E-132.05549E-11-2.25191E-114.38252E-12-1.26250E-7
A24.18410E-111.21370E-91.36996E-7-7.96186E-75.81812E-7-1.26250E-78.09476E-2
Date of computation: 2025-12-28 13:16 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: