2012TC4 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
1.620448
1-sigma variation
1.517E-7
Unit
Eccentricity (e)
Value
0.403762
1-sigma variation
4.391E-8
Unit
-
Inclination (i)
Value
0.5343
1-sigma variation
2.409E-6
Unit
Long. of Ascending Node (Ω)
Value
19.6950
1-sigma variation
3.925E-6
Unit
Arg. of Perihelion (ω)
Value
26.5760
1-sigma variation
9.095E-6
Unit
Mean Anomaly (M)
Value
324.44176
1-sigma variation
0.00020
Unit
Perihelion distance
Value
0.966172
1-sigma variation
Unit
Aphelion distance
Value
2.274724
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.001263
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.118137
1-sigma variation
Unit
MOID
Value
0.000100
1-sigma variation
Unit
Orbit Period
Value
753.4444
1-sigma variation
Unit
U parameter
Value
1.8
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a2.30009E-146.65023E-159.49437E-15-1.67418E-13-1.28781E-12-2.97647E-11
e6.65023E-151.92790E-15-1.97069E-16-4.38400E-14-3.73506E-13-8.60709E-12
i9.49437E-15-1.97069E-165.80454E-12-9.04477E-126.57686E-12-1.16007E-11
Ω-1.67418E-13-4.38400E-14-9.04477E-121.54048E-11-1.89963E-122.15580E-10
ω-1.28781E-12-3.73506E-136.57686E-12-1.89963E-128.27255E-111.66675E-9
M-2.97647E-11-8.60709E-12-1.16007E-112.15580E-101.66675E-93.85178E-8
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: