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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .1639317601525826 | 5.0072e-08 | |
| a | 3.194563229630291 | 2.4094e-08 | au |
| q | 2.670872856478279 | 1.6577e-07 | au |
| i | 16.91090342852724 | 8.953e-06 | deg |
| node | 317.4328512792295 | 1.4236e-05 | deg |
| peri | 131.5737383223254 | 3.1945e-05 | deg |
| M | 255.3564888910785 | 2.6959e-05 | deg |
| tp | 2459606.713302297779
(2022-Jan-27.21330230) | 0.00015752 | TDB |
| period | 2085.52624538794
5.71 | 2.3594e-05
6.46e-08 | d
yr |
| n | .1726183023570794 | 1.9529e-09 | deg/d |
| Q | 3.718253602782304 | 2.8044e-08 | au |
|
| | Orbit Determination Parameters
Additional Information
|
[ show covariance matrix ]
Physical Parameter Table
| Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
| absolute magnitude |
H |
13.6 |
|
n/a |
MPO445709 |
|
|
| 78912 (2003 SK99) Discovered 2003-Sep-19 by NEAT at Haleakala |
| Reference: 20040415/Numbers.arc | Last Updated: 2004-04-19 |
|
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