2017QC36 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
0.799170
1-sigma variation
3.311E-9
Unit
Eccentricity (e)
Value
0.296171
1-sigma variation
8.657E-8
Unit
-
Inclination (i)
Value
17.3563
1-sigma variation
0.0001
Unit
Long. of Ascending Node (Ω)
Value
136.6600
1-sigma variation
1.450E-5
Unit
Arg. of Perihelion (ω)
Value
356.5766
1-sigma variation
2.597E-5
Unit
Mean Anomaly (M)
Value
49.03977
1-sigma variation
0.00004
Unit
Perihelion distance
Value
0.562478
1-sigma variation
Unit
Aphelion distance
Value
1.035861
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.423928
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.020215
1-sigma variation
Unit
MOID
Value
0.020180
1-sigma variation
Unit
Orbit Period
Value
260.9497
1-sigma variation
Unit
U parameter
Value
0.5
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a1.09648E-171.61720E-161.16908E-133.09953E-14-2.20779E-14-1.15833E-14
e1.61720E-167.49444E-153.49717E-129.01579E-13-1.08795E-121.44533E-12
i1.16908E-133.49717E-122.59196E-96.24877E-10-3.46326E-102.63872E-10
Ω3.09953E-149.01579E-136.24877E-102.10263E-10-1.65168E-108.26039E-11
ω-2.20779E-14-1.08795E-12-3.46326E-10-1.65168E-106.74239E-10-9.09731E-10
M-1.15833E-141.44533E-122.63872E-108.26039E-11-9.09731E-101.62876E-9
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: