2013LX28 help
Last update: 2025-06-01 12:52 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
1.001654
1-sigma variation
7.358E-9
Unit
Eccentricity (e)
Value
0.451947
1-sigma variation
0.000001
Unit
-
Inclination (i)
Value
49.9808
1-sigma variation
0.0001
Unit
Long. of Ascending Node (Ω)
Value
76.6642
1-sigma variation
1.106E-5
Unit
Arg. of Perihelion (ω)
Value
345.7769
1-sigma variation
0.0001
Unit
Mean Anomaly (M)
Value
164.44579
1-sigma variation
0.00024
Unit
Perihelion distance
Value
0.548960
1-sigma variation
Unit
Aphelion distance
Value
1.454347
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.430945
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
0.403860
1-sigma variation
Unit
MOID
Value
0.374485
1-sigma variation
Unit
Orbit Period
Value
366.1632
1-sigma variation
Unit
U parameter
Value
1.3
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a5.41394E-175.14539E-154.21409E-13-4.26108E-14-8.68782E-142.44891E-13
e5.14539E-156.08637E-134.23221E-11-4.14239E-12-2.29957E-116.23604E-11
i4.21409E-134.23221E-118.96888E-9-9.67355E-105.14460E-9-1.08599E-8
Ω-4.26108E-14-4.14239E-12-9.67355E-101.22413E-10-6.83447E-101.45235E-9
ω-8.68782E-14-2.29957E-115.14460E-9-6.83447E-101.06871E-8-2.47217E-8
M2.44891E-136.23604E-11-1.08599E-81.45235E-9-2.47217E-85.75754E-8
Date of computation: 2025-06-01 12:52 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: