2015YQ1 help
Last update: 2025-04-04 18:16 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
1.004551
1-sigma variation
0.000011
Unit
Eccentricity (e)
Value
0.403918
1-sigma variation
0.000161
Unit
-
Inclination (i)
Value
2.4863
1-sigma variation
0.0014
Unit
Long. of Ascending Node (Ω)
Value
88.6646
1-sigma variation
0.0003
Unit
Arg. of Perihelion (ω)
Value
111.9438
1-sigma variation
0.0134
Unit
Mean Anomaly (M)
Value
49.57079
1-sigma variation
0.00973
Unit
Perihelion distance
Value
0.598795
1-sigma variation
Unit
Aphelion distance
Value
1.410307
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
0.006810
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.285848
1-sigma variation
Unit
MOID
Value
0.000669
1-sigma variation
Unit
Orbit Period
Value
367.7534
1-sigma variation
Unit
U parameter
Value
5.4
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.26614E-10-1.81501E-9-1.56706E-83.45905E-9-1.50197E-7-1.09443E-7
e-1.81501E-92.60278E-82.24725E-7-4.96502E-82.15381E-61.56955E-6
i-1.56706E-82.24725E-71.94062E-6-4.28737E-71.85961E-51.35517E-5
Ω3.45905E-9-4.96502E-8-4.28737E-79.50067E-8-4.10839E-6-2.99465E-6
ω-1.50197E-72.15381E-61.85961E-5-4.10839E-61.78229E-41.29881E-4
M-1.09443E-71.56955E-61.35517E-5-2.99465E-61.29881E-49.46505E-5
Date of computation: 2025-03-29 00:36 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: