1862 Apollo help
Last update: 2025-05-21 08:47 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
3.063E-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
1.172E-5
Unit
Arg. of Perihelion (ω)
Value
286.0250
1-sigma variation
1.223E-5
Unit
Mean Anomaly (M)
Value
3.39936
1-sigma variation
2.068E-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
-3.75224
1-sigma variation
0.28504
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.38102E-20-7.20791E-19-1.58923E-16-3.08465E-153.24842E-15-5.33005E-163.83471E-11
e-7.20791E-195.86433E-17-1.04568E-152.09702E-14-3.27500E-148.43238E-151.22035E-9
i-1.58923E-16-1.04568E-155.70761E-127.74525E-12-7.17333E-12-8.78724E-131.40705E-7
Ω-3.08465E-152.09702E-147.74525E-121.37456E-10-1.42312E-102.01867E-11-7.92869E-7
ω3.24842E-15-3.27500E-14-7.17333E-12-1.42312E-101.49622E-10-2.21429E-115.77414E-7
M-5.33005E-168.43238E-15-8.78724E-132.01867E-11-2.21429E-114.27685E-12-1.21963E-7
A23.83471E-111.22035E-91.40705E-7-7.92869E-75.77414E-7-1.21963E-78.12467E-2
Date of computation: 2025-05-21 08:47 UTC
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