2022AE1 help
Last update: 2025-02-19 13:28 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
1.469883
1-sigma variation
2.162E-8
Unit
Eccentricity (e)
Value
0.545839
1-sigma variation
5.004E-8
Unit
-
Inclination (i)
Value
6.2985
1-sigma variation
1.335E-5
Unit
Long. of Ascending Node (Ω)
Value
102.1766
1-sigma variation
9.224E-6
Unit
Arg. of Perihelion (ω)
Value
268.3812
1-sigma variation
8.737E-6
Unit
Mean Anomaly (M)
Value
342.73107
1-sigma variation
0.00001
Unit
Perihelion distance
Value
0.667563
1-sigma variation
Unit
Aphelion distance
Value
2.272202
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
0.064045
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.000366
1-sigma variation
Unit
MOID
Value
0.000073
1-sigma variation
Unit
Orbit Period
Value
650.9122
1-sigma variation
Unit
U parameter
Value
0.6
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a4.67385E-16-1.06575E-151.26095E-13-6.14908E-143.13461E-14-2.39612E-13
e-1.06575E-152.50382E-15-2.86522E-131.61904E-13-5.48440E-145.26531E-13
i1.26095E-13-2.86522E-131.78106E-10-1.19880E-111.78887E-11-6.98167E-11
Ω-6.14908E-141.61904E-13-1.19880E-118.50818E-11-3.57473E-111.28738E-11
ω3.13461E-14-5.48440E-141.78887E-11-3.57473E-117.63411E-11-3.38983E-11
M-2.39612E-135.26531E-13-6.98167E-111.28738E-11-3.38983E-111.38537E-10
Date of computation: 2025-02-19 13:28 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: