2022RM4 help
Last update: 2025-04-01 07:30 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
60800.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
2.454384
1-sigma variation
0.000005
Unit
Eccentricity (e)
Value
0.596806
1-sigma variation
0.000001
Unit
-
Inclination (i)
Value
38.2940
1-sigma variation
1.997E-5
Unit
Long. of Ascending Node (Ω)
Value
218.1405
1-sigma variation
1.055E-6
Unit
Arg. of Perihelion (ω)
Value
181.7428
1-sigma variation
4.478E-6
Unit
Mean Anomaly (M)
Value
234.22974
1-sigma variation
0.00068
Unit
Perihelion distance
Value
0.989592
1-sigma variation
Unit
Aphelion distance
Value
3.919176
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
2.909610
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.002856
1-sigma variation
Unit
MOID
Value
0.002862
1-sigma variation
Unit
Orbit Period
Value
1404.4691
1-sigma variation
Unit
U parameter
Value
3.3
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a2.25633E-113.70299E-129.38258E-11-4.67141E-12-6.51627E-12-3.22679E-9
e3.70299E-126.07727E-131.53996E-11-7.66599E-13-1.06229E-12-5.29567E-10
i9.38258E-111.53996E-113.98868E-10-1.98427E-11-2.51027E-11-1.34185E-8
Ω-4.67141E-12-7.66599E-13-1.98427E-111.11360E-121.19961E-126.68083E-10
ω-6.51627E-12-1.06229E-12-2.51027E-111.19961E-122.00491E-119.28184E-10
M-3.22679E-9-5.29567E-10-1.34185E-86.68083E-109.28184E-104.61465E-7
Date of computation: 2025-02-19 13:28 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: