1862 Apollo help
Last update: 2024-03-28 23:50 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
1.470569
1-sigma variation
2.959E-10
Unit
Eccentricity (e)
Value
0.559902
1-sigma variation
7.529E-9
Unit
-
Inclination (i)
Value
6.3525
1-sigma variation
2.379E-6
Unit
Long. of Ascending Node (Ω)
Value
35.5560
1-sigma variation
1.153E-5
Unit
Arg. of Perihelion (ω)
Value
286.0393
1-sigma variation
1.203E-5
Unit
Mean Anomaly (M)
Value
142.31869
1-sigma variation
1.985E-6
Unit
Perihelion distance
Value
0.647195
1-sigma variation
Unit
Aphelion distance
Value
2.293943
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.118458
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.188393
1-sigma variation
Unit
MOID
Value
0.025860
1-sigma variation
Unit
Orbit Period
Value
651.3679
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
A2
Value
-3.71855
1-sigma variation
0.28144
Unit
10-15au/days2
Covariance Matrix
aeiΩωMA2
a8.75803E-20-7.53195E-19-1.60091E-16-2.95824E-153.12681E-15-4.90943E-163.36031E-11
e-7.53195E-195.66860E-17-1.07741E-152.06203E-14-3.20230E-148.05440E-151.17339E-9
i-1.60091E-16-1.07741E-155.65752E-127.45937E-12-6.88140E-12-9.44641E-131.41470E-7
Ω-2.95824E-152.06203E-147.45937E-121.32832E-10-1.37602E-101.88870E-11-7.61632E-7
ω3.12681E-15-3.20230E-14-6.88140E-12-1.37602E-101.44752E-10-2.07621E-115.55006E-7
M-4.90943E-168.05440E-15-9.44641E-131.88870E-11-2.07621E-113.93886E-12-1.11775E-7
A23.36031E-111.17339E-91.41470E-7-7.61632E-75.55006E-7-1.11775E-77.92075E-2
Date of computation: 2024-02-25 11:58 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: