2015HM10 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
2.539035
1-sigma variation
3.430E-9
Unit
Eccentricity (e)
Value
0.603637
1-sigma variation
2.632E-9
Unit
-
Inclination (i)
Value
1.4976
1-sigma variation
2.206E-6
Unit
Long. of Ascending Node (Ω)
Value
282.4355
1-sigma variation
1.532E-5
Unit
Arg. of Perihelion (ω)
Value
354.7489
1-sigma variation
1.658E-5
Unit
Mean Anomaly (M)
Value
159.70096
1-sigma variation
1.232E-6
Unit
Perihelion distance
Value
1.006379
1-sigma variation
Unit
Aphelion distance
Value
4.071690
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.008227
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
3.060450
1-sigma variation
Unit
MOID
Value
0.003337
1-sigma variation
Unit
Orbit Period
Value
1477.7514
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.17623E-172.48226E-19-7.95837E-167.94854E-15-2.33094E-143.09111E-15
e2.48226E-196.92952E-182.00307E-162.99567E-164.01239E-15-1.85899E-15
i-7.95837E-162.00307E-164.86579E-121.41241E-11-1.46191E-114.05018E-13
Ω7.94854E-152.99567E-161.41241E-112.34584E-10-2.42176E-108.22153E-13
ω-2.33094E-144.01239E-15-1.46191E-11-2.42176E-102.74974E-10-6.66515E-12
M3.09111E-15-1.85899E-154.05018E-138.22153E-13-6.66515E-121.51906E-12
Date of computation: 2025-03-29 00:36 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: