1862 Apollo
Last update: 2021-10-18 13:09 UTC
Epoch
Orbit properties
  • Epoch
  • Semimajor Axis
  • Eccentricity (e)
  • Inclination (i)
  • Ascending Node (Ω)
  • Arg. of Perihelion (ω)
  • Mean Anomaly (M)
  • Perihelion
  • Aphelion
  • Asc. Node-Earth Sep.
  • Desc. Node-Earth Sep.
  • MOID
  • Orbit Period
Value
1-sigma variation
Unit
Epoch
Value
59400.0
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.47
1-sigma variation
7.69188E-10
Unit
Eccentricity (e)
Value
0.560003290270412
1-sigma variation
1.1693E-8
Unit
-
Inclination (i)
Value
6.36
1-sigma variation
2.982E-6
Unit
Ascending Node (Ω)
Value
35.61
1-sigma variation
2.170E-5
Unit
Arg. of Perihelion (ω)
Value
286.01
1-sigma variation
2.256E-5
Unit
Mean Anomaly (M)
Value
309.64
1-sigma variation
3.372E-6
Unit
Perihelion
Value
6.469E-1
1-sigma variation
Unit
Aphelion
Value
2.29
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-1.203E-1
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.877E-1
1-sigma variation
Unit
MOID
Value
2.626E-2
1-sigma variation
Unit
Orbit Period
Value
651.16
1-sigma variation
Unit
A2
Value
-3.72829
1-sigma variation
0.41289
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a5.91651E-19-4.12301E-184.81629E-16-1.50390E-141.60529E-14-2.57684E-151.31572E-10
e-4.12301E-181.36726E-16-3.27289E-156.06172E-14-8.85702E-141.99938E-142.70433E-9
i4.81629E-16-3.27289E-158.89235E-129.48696E-12-8.24099E-12-2.02307E-122.11693E-7
Ω-1.50390E-146.06172E-149.48696E-124.70858E-10-4.87020E-106.59111E-11-4.15023E-6
ω1.60529E-14-8.85702E-14-8.24099E-12-4.87020E-105.09035E-10-7.07485E-113.67971E-6
M-2.57684E-151.99938E-14-2.02307E-126.59111E-11-7.07485E-111.13701E-11-4.65239E-7
A21.31572E-102.70433E-92.11693E-7-4.15023E-63.67971E-6-4.65239E-71.70475E-1
Date of computation: 2021-10-04 23:49 UTC
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