719 Albert help
Last update: 2026-06-05 09:04 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
61200.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
2.636950
1-sigma variation
2.379E-9
Unit
Eccentricity (e)
Value
0.546593
1-sigma variation
1.935E-8
Unit
-
Inclination (i)
Value
11.5724
1-sigma variation
2.598E-6
Unit
Long. of Ascending Node (Ω)
Value
183.8603
1-sigma variation
1.352E-5
Unit
Arg. of Perihelion (ω)
Value
156.1760
1-sigma variation
1.370E-5
Unit
Mean Anomaly (M)
Value
286.67722
1-sigma variation
2.940E-6
Unit
Perihelion distance
Value
1.195612
1-sigma variation
Unit
Aphelion distance
Value
4.078287
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
2.701182
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.229822
1-sigma variation
Unit
MOID
Value
0.201591
1-sigma variation
Unit
Orbit Period
Value
1564.0519
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a5.66023E-18-2.27913E-171.63553E-152.19118E-151.18255E-15-6.34889E-15
e-2.27913E-173.74437E-16-1.04256E-14-1.59156E-141.65866E-142.88769E-14
i1.63553E-15-1.04256E-146.75106E-12-2.45970E-123.37735E-12-2.05827E-12
Ω2.19118E-15-1.59156E-14-2.45970E-121.82796E-10-1.79172E-10-1.28266E-12
ω1.18255E-151.65866E-143.37735E-12-1.79172E-101.87596E-10-4.85919E-12
M-6.34889E-152.88769E-14-2.05827E-12-1.28266E-12-4.85919E-128.64197E-12
Date of computation: 2026-06-05 09:04 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: