2058 Roka help
Last update: 2024-05-21 12:25 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
60400.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
3.125046
1-sigma variation
9.941E-9
Unit
Eccentricity (e)
Value
0.145322
1-sigma variation
2.260E-8
Unit
-
Inclination (i)
Value
2.5350
1-sigma variation
2.632E-6
Unit
Long. of Ascending Node (Ω)
Value
95.3019
1-sigma variation
0.0001
Unit
Arg. of Perihelion (ω)
Value
181.4387
1-sigma variation
0.0001
Unit
Mean Anomaly (M)
Value
84.63616
1-sigma variation
0.00001
Unit
Perihelion distance
Value
2.670907
1-sigma variation
Unit
Aphelion distance
Value
3.579184
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
2.596203
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.654473
1-sigma variation
Unit
MOID
Value
1.654298
1-sigma variation
Unit
Orbit Period
Value
2017.8225
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a9.88216E-171.52267E-172.20012E-174.64957E-16-3.07910E-149.71480E-15
e1.52267E-175.10806E-16-4.95789E-17-1.88461E-152.79816E-14-2.29274E-14
i2.20012E-17-4.95789E-176.92906E-122.26450E-11-2.26467E-111.81354E-14
Ω4.64957E-16-1.88461E-152.26450E-114.98238E-9-4.97671E-9-7.34071E-13
ω-3.07910E-142.79816E-14-2.26467E-11-4.97671E-95.10594E-9-1.21922E-10
M9.71480E-15-2.29274E-141.81354E-14-7.34071E-13-1.21922E-101.19137E-10
Date of computation: 2024-04-23 10:11 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: