2012TC4 help
Last update: 2024-05-06 05:00 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
1.620313
1-sigma variation
1.515E-7
Unit
Eccentricity (e)
Value
0.403966
1-sigma variation
4.415E-8
Unit
-
Inclination (i)
Value
0.5345
1-sigma variation
2.410E-6
Unit
Long. of Ascending Node (Ω)
Value
19.7059
1-sigma variation
3.936E-6
Unit
Arg. of Perihelion (ω)
Value
26.5418
1-sigma variation
9.040E-6
Unit
Mean Anomaly (M)
Value
37.79338
1-sigma variation
0.00016
Unit
Perihelion distance
Value
0.965762
1-sigma variation
Unit
Aphelion distance
Value
2.274864
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.000725
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.119648
1-sigma variation
Unit
MOID
Value
0.000058
1-sigma variation
Unit
Orbit Period
Value
753.3500
1-sigma variation
Unit
U parameter
Value
1.8
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a2.29485E-146.67915E-159.46744E-15-1.68938E-13-1.27693E-12-2.36641E-11
e6.67915E-151.94906E-15-1.79376E-16-4.46051E-14-3.72822E-13-6.88865E-12
i9.46744E-15-1.79376E-165.80662E-12-9.06696E-126.60406E-12-9.08125E-12
Ω-1.68938E-13-4.46051E-14-9.06696E-121.54915E-11-1.92947E-121.73140E-10
ω-1.27693E-12-3.72822E-136.60406E-12-1.92947E-128.17226E-111.31699E-9
M-2.36641E-11-6.88865E-12-9.08125E-121.73140E-101.31699E-92.44023E-8
Date of computation: 2024-04-23 10:08 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: