2023GQ2 help
Last update: 2025-09-10 00:30 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
61000.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.644300
1-sigma variation
9.171E-8
Unit
Eccentricity (e)
Value
0.401690
1-sigma variation
0.000001
Unit
-
Inclination (i)
Value
36.8412
1-sigma variation
0.0001
Unit
Long. of Ascending Node (Ω)
Value
53.8250
1-sigma variation
0.0001
Unit
Arg. of Perihelion (ω)
Value
349.3688
1-sigma variation
0.0001
Unit
Mean Anomaly (M)
Value
213.81599
1-sigma variation
0.00031
Unit
Perihelion distance
Value
0.983802
1-sigma variation
Unit
Aphelion distance
Value
2.304799
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.000335
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
1.266178
1-sigma variation
Unit
MOID
Value
0.000333
1-sigma variation
Unit
Orbit Period
Value
770.1407
1-sigma variation
Unit
U parameter
Value
1.7
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a8.41109E-153.04844E-14-5.75791E-125.66180E-126.91914E-12-2.77454E-11
e3.04844E-145.94972E-13-5.20967E-116.21934E-11-2.03333E-11-1.23244E-10
i-5.75791E-12-5.20967E-118.73531E-9-9.53264E-93.77276E-102.07530E-8
Ω5.66180E-126.21934E-11-9.53264E-91.08732E-8-1.84266E-9-2.09217E-8
ω6.91914E-12-2.03333E-113.77276E-10-1.84266E-91.21812E-8-2.08485E-8
M-2.77454E-11-1.23244E-102.07530E-8-2.09217E-8-2.08485E-89.32095E-8
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: