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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 3 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .1042485092264387 | 3.3566e-07 | |
a | 5.15486608912201 | 1.0656e-06 | au |
q | 4.617478984069119 | 2.6636e-06 | au |
i | 17.83830707918584 | 9.2328e-06 | deg |
node | 297.0252286853056 | 5.6821e-05 | deg |
peri | 358.6983877924487 | 0.00010174 | deg |
M | 291.3747075432686 | 0.00010222 | deg |
tp | 2459815.403562024379 (2022-Aug-23.90356202) | 0.0013761 | TDB |
period | 4274.885713802164 11.70 | 0.0013256 3.629e-06 | d yr |
n | .08421277762764076 | 2.6113e-08 | deg/d |
Q | 5.692253194174902 | 1.1767e-06 | 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 |
13.949 |
|
.33565 |
3 |
autocmod 2.8 |
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