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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 24 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .1050967688998546 | 5.5305e-08 | |
| a | 3.207634399651844 | 3.1891e-08 | au |
| q | 2.87052238843641 | 1.8217e-07 | au |
| i | 14.30310676566682 | 4.5947e-06 | deg |
| node | 233.6048199419596 | 2.3493e-05 | deg |
| peri | 257.4600704478968 | 3.4737e-05 | deg |
| M | 201.6770617300367 | 2.8097e-05 | deg |
| tp | 2459923.320132892992
(2022-Dec-09.82013289) | 0.00016974 | TDB |
| period | 2098.339327653221
5.74 | 3.1293e-05
8.568e-08 | d
yr |
| n | .1715642438073271 | 2.5586e-09 | deg/d |
| Q | 3.544746410867277 | 3.5243e-08 | au |
|
| | Orbit Determination Parameters
Additional Information
|
[ show covariance matrix ]
Physical Parameter Table
| Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
| absolute magnitude |
H |
14.3 |
|
n/a |
MPO439584 |
|
|
| 78970 (2003 SB298) Discovered 2003-Sep-18 by NEAT at Haleakala |
| Reference: 20040415/Numbers.arc | Last Updated: 2004-04-19 |
|
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