2006QV89 help
Last update: 2025-03-31 10:04 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
1.192877
1-sigma variation
9.105E-9
Unit
Eccentricity (e)
Value
0.224699
1-sigma variation
0.000001
Unit
-
Inclination (i)
Value
1.0688
1-sigma variation
5.877E-6
Unit
Long. of Ascending Node (Ω)
Value
165.8769
1-sigma variation
4.063E-5
Unit
Arg. of Perihelion (ω)
Value
236.5312
1-sigma variation
0.0002
Unit
Mean Anomaly (M)
Value
82.39894
1-sigma variation
0.00009
Unit
Perihelion distance
Value
0.924838
1-sigma variation
Unit
Aphelion distance
Value
1.460916
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
0.299864
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.001044
1-sigma variation
Unit
MOID
Value
0.000126
1-sigma variation
Unit
Orbit Period
Value
475.8739
1-sigma variation
Unit
U parameter
Value
0.6
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a8.28955E-17-4.93198E-15-3.65595E-143.70823E-15-1.63576E-128.57464E-13
e-4.93198E-152.98161E-132.19502E-12-4.06008E-139.87323E-11-5.15207E-11
i-3.65595E-142.19502E-123.45414E-11-1.37890E-108.63385E-10-3.80625E-10
Ω3.70823E-15-4.06008E-13-1.37890E-101.65088E-9-1.70995E-93.98743E-12
ω-1.63576E-129.87323E-118.63385E-10-1.70995E-93.42836E-8-1.70714E-8
M8.57464E-13-5.15207E-11-3.80625E-103.98743E-12-1.70714E-88.96951E-9
Date of computation: 2025-03-31 10:04 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: