2016EU85 help
Last update: 2025-03-29 00:36 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
1.848183
1-sigma variation
6.421E-8
Unit
Eccentricity (e)
Value
0.482113
1-sigma variation
3.326E-7
Unit
-
Inclination (i)
Value
2.5938
1-sigma variation
1.971E-5
Unit
Long. of Ascending Node (Ω)
Value
359.3680
1-sigma variation
0.0002
Unit
Arg. of Perihelion (ω)
Value
23.5928
1-sigma variation
0.0002
Unit
Mean Anomaly (M)
Value
321.68351
1-sigma variation
0.00005
Unit
Perihelion distance
Value
0.957149
1-sigma variation
Unit
Aphelion distance
Value
2.739217
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.019493
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.545684
1-sigma variation
Unit
MOID
Value
0.006103
1-sigma variation
Unit
Orbit Period
Value
917.7319
1-sigma variation
Unit
U parameter
Value
1.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a4.12320E-151.39903E-161.54573E-141.00710E-13-2.21900E-12-9.18235E-13
e1.39903E-161.10648E-135.32379E-14-5.21418E-13-1.21995E-12-1.19138E-11
i1.54573E-145.32379E-143.88507E-10-2.72879E-92.71546E-9-5.70524E-12
Ω1.00710E-13-5.21418E-13-2.72879E-93.14154E-8-3.14638E-88.47710E-11
ω-2.21900E-12-1.21995E-122.71546E-9-3.14638E-83.31291E-8-1.62787E-10
M-9.18235E-13-1.19138E-11-5.70524E-128.47710E-11-1.62787E-102.58613E-9
Date of computation: 2025-03-29 00:36 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: