3102 Krok help
Last update: 2025-07-15 12:54 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
2.151336
1-sigma variation
1.402E-9
Unit
Eccentricity (e)
Value
0.449228
1-sigma variation
1.305E-8
Unit
-
Inclination (i)
Value
8.4425
1-sigma variation
1.866E-6
Unit
Long. of Ascending Node (Ω)
Value
172.0498
1-sigma variation
1.420E-5
Unit
Arg. of Perihelion (ω)
Value
154.7535
1-sigma variation
1.432E-5
Unit
Mean Anomaly (M)
Value
304.27996
1-sigma variation
2.151E-6
Unit
Perihelion distance
Value
1.184896
1-sigma variation
Unit
Aphelion distance
Value
3.117776
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
1.898495
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.215647
1-sigma variation
Unit
MOID
Value
0.184482
1-sigma variation
Unit
Orbit Period
Value
1152.5525
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.96645E-18-4.63346E-181.85435E-167.31591E-16-5.06721E-16-1.02854E-15
e-4.63346E-181.70402E-16-2.06970E-15-2.69159E-152.52243E-156.68537E-15
i1.85435E-16-2.06970E-153.48064E-121.39974E-12-6.03699E-13-7.18274E-13
Ω7.31591E-16-2.69159E-151.39974E-122.01662E-10-1.96770E-10-2.16946E-12
ω-5.06721E-162.52243E-15-6.03699E-13-1.96770E-102.04946E-10-4.43775E-12
M-1.02854E-156.68537E-15-7.18274E-13-2.16946E-12-4.43775E-124.62628E-12
Date of computation: 2025-07-15 12:54 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: