2015YA help
Last update: 2026-06-04 23:11 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
0.995170
1-sigma variation
0.000002
Unit
Eccentricity (e)
Value
0.279703
1-sigma variation
0.000210
Unit
-
Inclination (i)
Value
1.6182
1-sigma variation
0.0008
Unit
Long. of Ascending Node (Ω)
Value
254.8623
1-sigma variation
0.0033
Unit
Arg. of Perihelion (ω)
Value
83.4652
1-sigma variation
0.0160
Unit
Mean Anomaly (M)
Value
270.12002
1-sigma variation
0.08992
Unit
Perihelion distance
Value
0.716818
1-sigma variation
Unit
Aphelion distance
Value
1.273523
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.126123
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.037532
1-sigma variation
Unit
MOID
Value
0.003616
1-sigma variation
Unit
Orbit Period
Value
362.6140
1-sigma variation
Unit
U parameter
Value
5.1
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a5.96022E-125.12274E-101.92270E-97.82956E-9-3.90071E-8-2.19519E-7
e5.12274E-104.40434E-81.65251E-76.72303E-7-3.35290E-6-1.88677E-5
i1.92270E-91.65251E-76.24335E-72.55753E-6-1.26136E-5-7.08272E-5
Ω7.82956E-96.72303E-72.55753E-61.05644E-5-5.14683E-5-2.88461E-4
ω-3.90071E-8-3.35290E-6-1.26136E-5-5.14683E-52.55521E-41.43676E-3
M-2.19519E-7-1.88677E-5-7.08272E-5-2.88461E-41.43676E-38.08511E-3
Date of computation: 2026-06-04 23:11 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: