5786 Talos help
Last update: 2025-07-29 02:36 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
1.081541
1-sigma variation
1.389E-9
Unit
Eccentricity (e)
Value
0.826787
1-sigma variation
2.367E-8
Unit
-
Inclination (i)
Value
23.2204
1-sigma variation
5.638E-6
Unit
Long. of Ascending Node (Ω)
Value
161.2797
1-sigma variation
5.463E-6
Unit
Arg. of Perihelion (ω)
Value
8.3883
1-sigma variation
6.568E-6
Unit
Mean Anomaly (M)
Value
92.82422
1-sigma variation
0.00001
Unit
Perihelion distance
Value
0.187337
1-sigma variation
Unit
Aphelion distance
Value
1.975745
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.803127
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.871455
1-sigma variation
Unit
MOID
Value
0.188661
1-sigma variation
Unit
Orbit Period
Value
410.8306
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.92908E-18-8.96931E-184.83847E-163.06372E-16-2.05514E-17-7.46378E-15
e-8.96931E-185.60413E-161.30158E-141.10874E-14-2.39473E-144.82460E-14
i4.83847E-161.30158E-143.17867E-116.68001E-12-7.49582E-122.99878E-12
Ω3.06372E-161.10874E-146.68001E-122.98484E-11-3.19116E-111.24414E-11
ω-2.05514E-17-2.39473E-14-7.49582E-12-3.19116E-114.31439E-11-3.00388E-11
M-7.46378E-154.82460E-142.99878E-121.24414E-11-3.00388E-118.03451E-11
Date of computation: 2025-07-29 02:36 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: