1862 Apollo help
Last update: 2025-03-29 00:36 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
60800.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.470719
1-sigma variation
3.062E-10
Unit
Eccentricity (e)
Value
0.559846
1-sigma variation
7.658E-9
Unit
-
Inclination (i)
Value
6.3522
1-sigma variation
2.389E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5571
1-sigma variation
1.171E-5
Unit
Arg. of Perihelion (ω)
Value
286.0250
1-sigma variation
1.222E-5
Unit
Mean Anomaly (M)
Value
3.39936
1-sigma variation
2.066E-6
Unit
Perihelion distance
Value
0.647342
1-sigma variation
Unit
Aphelion distance
Value
2.294095
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.118819
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.188355
1-sigma variation
Unit
MOID
Value
0.025962
1-sigma variation
Unit
Orbit Period
Value
651.4676
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
A2
Value
-3.75229
1-sigma variation
0.28504
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.37757E-20-7.20880E-19-1.59155E-16-3.08147E-153.24523E-15-5.32492E-163.83464E-11
e-7.20880E-195.86429E-17-1.04640E-152.09795E-14-3.27592E-148.43386E-151.22036E-9
i-1.59155E-16-1.04640E-155.70599E-127.76713E-12-7.19529E-12-8.75193E-131.40706E-7
Ω-3.08147E-152.09795E-147.76713E-121.37158E-10-1.42014E-102.01387E-11-7.92850E-7
ω3.24523E-15-3.27592E-14-7.19529E-12-1.42014E-101.49323E-10-2.20947E-115.77393E-7
M-5.32492E-168.43386E-15-8.75193E-132.01387E-11-2.20947E-114.26910E-12-1.21960E-7
A23.83464E-111.22036E-91.40706E-7-7.92850E-75.77393E-7-1.21960E-78.12463E-2
Date of computation: 2025-03-28 15:40 UTC
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