242450 2004QY2 help
Last update: 2026-07-30 09:40 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
1.083886
1-sigma variation
2.649E-9
Unit
Eccentricity (e)
Value
0.477102
1-sigma variation
3.594E-8
Unit
-
Inclination (i)
Value
37.0332
1-sigma variation
6.834E-6
Unit
Long. of Ascending Node (Ω)
Value
295.2718
1-sigma variation
7.204E-6
Unit
Arg. of Perihelion (ω)
Value
104.9856
1-sigma variation
8.230E-6
Unit
Mean Anomaly (M)
Value
38.79575
1-sigma variation
0.00001
Unit
Perihelion distance
Value
0.566763
1-sigma variation
Unit
Aphelion distance
Value
1.601010
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.061584
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.238547
1-sigma variation
Unit
MOID
Value
0.046980
1-sigma variation
Unit
Orbit Period
Value
412.1679
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a7.01697E-189.74998E-182.19672E-162.01046E-15-1.66244E-15-1.79350E-14
e9.74998E-181.29160E-154.18505E-146.57985E-14-6.97341E-149.92346E-14
i2.19672E-164.18505E-144.67032E-11-6.53908E-13-2.12009E-125.99075E-12
Ω2.01046E-156.57985E-14-6.53908E-135.18914E-11-3.48455E-11-2.04915E-11
ω-1.66244E-15-6.97341E-14-2.12009E-12-3.48455E-116.77275E-11-2.04381E-11
M-1.79350E-149.92346E-145.99075E-12-2.04915E-11-2.04381E-119.08576E-11
Date of computation: 2026-07-30 09:40 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: