2015DR215 help
Last update: 2025-01-30 14:31 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
60600.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
0.666644
1-sigma variation
3.362E-9
Unit
Eccentricity (e)
Value
0.471506
1-sigma variation
5.435E-8
Unit
-
Inclination (i)
Value
4.0552
1-sigma variation
1.401E-5
Unit
Long. of Ascending Node (Ω)
Value
314.5663
1-sigma variation
0.0002
Unit
Arg. of Perihelion (ω)
Value
42.6967
1-sigma variation
0.0002
Unit
Mean Anomaly (M)
Value
85.35407
1-sigma variation
0.00003
Unit
Perihelion distance
Value
0.352317
1-sigma variation
Unit
Aphelion distance
Value
0.980970
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.628656
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.190636
1-sigma variation
Unit
MOID
Value
0.043686
1-sigma variation
Unit
Orbit Period
Value
198.8103
1-sigma variation
Unit
U parameter
Value
0.8
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.13036E-178.46505E-173.49428E-145.97889E-13-6.17779E-133.47962E-15
e8.46505E-172.95381E-152.55589E-135.13605E-12-5.08160E-12-4.72512E-13
i3.49428E-142.55589E-131.96165E-102.75356E-9-2.81610E-91.84933E-11
Ω5.97889E-135.13605E-122.75356E-94.31429E-8-4.42740E-85.06371E-10
ω-6.17779E-13-5.08160E-12-2.81610E-9-4.42740E-84.56040E-8-9.13570E-10
M3.47962E-15-4.72512E-131.84933E-115.06371E-10-9.13570E-101.00433E-9
Date of computation: 2024-12-09 13:46 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: