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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 25 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .09146710447304837 | 4.6058e-08 | |
a | 2.985161888032069 | 2.3111e-08 | au |
q | 2.712117773750478 | 1.3501e-07 | au |
i | 9.85715744612008 | 4.6434e-06 | deg |
node | 25.43225222835256 | 2.824e-05 | deg |
peri | 331.31544604 | 3.9145e-05 | deg |
M | 143.2032197743929 | 2.9207e-05 | deg |
tp | 2458251.122686397526 (2018-May-12.62268640) | 0.00015139 | TDB |
period | 1883.867089873429 5.16 | 2.1878e-05 5.99e-08 | d yr |
n | .1910962837745561 | 2.2192e-09 | deg/d |
Q | 3.258206002313661 | 2.5225e-08 | au |
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| | Orbit Determination Parameters
Additional Information
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[ show covariance matrix ]
Physical Parameter Table
Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
absolute magnitude |
H |
14.6 |
|
n/a |
MPO412654 |
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|
78659 (2002 TD79) Discovered 2002-Oct-01 by NEAT at Haleakala |
Reference: 20040415/Numbers.arc | Last Updated: 2004-04-19 |
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