1862 Apollo help
Last update: 2026-03-10 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
7.594E-9
Unit
-
Inclination (i)
Value
6.3522
1-sigma variation
2.280E-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
1.219E-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
-3.76674
1-sigma variation
0.28313
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a9.53111E-20-5.95914E-19-1.41074E-16-3.07186E-153.21197E-15-5.49626E-164.36693E-11
e-5.95914E-195.76634E-17-9.51305E-162.13499E-14-3.29175E-148.48999E-151.19277E-9
i-1.41074E-16-9.51305E-165.19811E-126.93553E-12-6.41886E-12-7.79844E-131.30092E-7
Ω-3.07186E-152.13499E-146.93553E-121.36179E-10-1.41149E-102.09646E-11-8.04562E-7
ω3.21197E-15-3.29175E-14-6.41886E-12-1.41149E-101.48525E-10-2.29281E-115.93878E-7
M-5.49626E-168.48999E-15-7.79844E-132.09646E-11-2.29281E-114.49401E-12-1.31999E-7
A24.36693E-111.19277E-91.30092E-7-8.04562E-75.93878E-7-1.31999E-78.01637E-2
Date of computation: 2026-03-10 13:00 UTC
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