2012KT42 help
Last update: 2024-03-28 23:50 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
60400.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.597820
1-sigma variation
0.000058
Unit
Eccentricity (e)
Value
0.554470
1-sigma variation
0.000034
Unit
-
Inclination (i)
Value
2.1932
1-sigma variation
0.0003
Unit
Long. of Ascending Node (Ω)
Value
69.4769
1-sigma variation
4.900E-5
Unit
Arg. of Perihelion (ω)
Value
259.1272
1-sigma variation
0.0023
Unit
Mean Anomaly (M)
Value
285.54084
1-sigma variation
0.12421
Unit
Perihelion distance
Value
0.711877
1-sigma variation
Unit
Aphelion distance
Value
2.483764
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
0.249229
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.011202
1-sigma variation
Unit
MOID
Value
0.000849
1-sigma variation
Unit
Orbit Period
Value
737.7180
1-sigma variation
Unit
U parameter
Value
6.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a3.41721E-91.97105E-9-1.72156E-82.50767E-91.34451E-7-7.26068E-6
e1.97105E-91.14027E-9-1.00448E-81.47682E-97.81831E-8-4.18800E-6
i-1.72156E-8-1.00448E-89.14921E-8-1.31829E-8-6.99399E-73.65795E-5
Ω2.50767E-91.47682E-9-1.31829E-82.40092E-91.04097E-7-5.32837E-6
ω1.34451E-77.81831E-8-6.99399E-71.04097E-75.40891E-6-2.85678E-4
M-7.26068E-6-4.18800E-63.65795E-5-5.32837E-6-2.85678E-41.54270E-2
Date of computation: 2024-02-21 14:29 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: