2022RM4 help
Last update: 2025-09-10 00:30 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
61000.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
2.454343
1-sigma variation
0.000005
Unit
Eccentricity (e)
Value
0.596741
1-sigma variation
0.000001
Unit
-
Inclination (i)
Value
38.2886
1-sigma variation
1.991E-5
Unit
Long. of Ascending Node (Ω)
Value
218.1353
1-sigma variation
1.037E-6
Unit
Arg. of Perihelion (ω)
Value
181.7485
1-sigma variation
4.498E-6
Unit
Mean Anomaly (M)
Value
285.48210
1-sigma variation
0.00083
Unit
Perihelion distance
Value
0.989736
1-sigma variation
Unit
Aphelion distance
Value
3.918951
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
2.907839
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.002898
1-sigma variation
Unit
MOID
Value
0.002897
1-sigma variation
Unit
Orbit Period
Value
1404.4341
1-sigma variation
Unit
U parameter
Value
3.3
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a2.25932E-113.70135E-129.35795E-11-4.58010E-12-6.80584E-12-3.93664E-9
e3.70135E-126.06387E-131.53321E-11-7.50289E-13-1.10779E-12-6.44926E-10
i9.35795E-111.53321E-113.96308E-10-1.93881E-11-2.61939E-11-1.63058E-8
Ω-4.58010E-12-7.50289E-13-1.93881E-111.07499E-121.22730E-127.98062E-10
ω-6.80584E-12-1.10779E-12-2.61939E-111.22730E-122.02307E-111.18212E-9
M-3.93664E-9-6.44926E-10-1.63058E-87.98062E-101.18212E-96.85923E-7
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: