2010JL88 help
Last update: 2025-06-12 08:28 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
1.425504
1-sigma variation
0.001698
Unit
Eccentricity (e)
Value
0.503869
1-sigma variation
0.000156
Unit
-
Inclination (i)
Value
0.0942
1-sigma variation
0.0018
Unit
Long. of Ascending Node (Ω)
Value
267.0168
1-sigma variation
1.5347
Unit
Arg. of Perihelion (ω)
Value
53.2674
1-sigma variation
1.6466
Unit
Mean Anomaly (M)
Value
260.33687
1-sigma variation
0.72639
Unit
Perihelion distance
Value
0.707237
1-sigma variation
Unit
Aphelion distance
Value
2.143771
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.210329
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.580739
1-sigma variation
Unit
MOID
Value
0.000909
1-sigma variation
Unit
Orbit Period
Value
621.6573
1-sigma variation
Unit
U parameter
Value
8.2
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a2.88276E-62.65184E-7-3.08456E-6-2.60558E-32.79552E-3-1.23331E-3
e2.65184E-72.43972E-8-2.83793E-7-2.39666E-42.57140E-4-1.13453E-4
i-3.08456E-6-2.83793E-73.30203E-62.78735E-3-2.99059E-31.31965E-3
Ω-2.60558E-3-2.39666E-42.78735E-32.35530E0-2.52697E01.11472E0
ω2.79552E-32.57140E-4-2.99059E-3-2.52697E02.71117E0-1.19598E0
M-1.23331E-3-1.13453E-41.31965E-31.11472E0-1.19598E05.27639E-1
Date of computation: 2025-06-12 08:28 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: