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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.
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Orbital Elements at Epoch 2457349.5 (2015-Nov-23.0) TDB
Reference: JPL 83 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | 1.000280834371231 | 1.4549e-06 | |
| a | -2930.444713296654 | 15.181 | au |
| q | .8229695984860307 | 2.8268e-07 | au |
| i | 148.8782906405183 | 8.6305e-06 | deg |
| node | 186.1445580421072 | 3.0725e-05 | deg |
| peri | 340.358747245559 | 3.5088e-05 | deg |
| M | 4.522064531657807E-5 | 3.513e-07 | deg |
| tp | 2457342.221649261460
(2015-Nov-15.72164926) | 2.0984e-05 | TDB |
| period | n/a
n/a | n/a
n/a | d
yr |
| n | 6.213034647688482E-6 | 4.828e-08 | deg/d |
| Q | n/a | n/a | au |
|
Additional Model Parameters
| Parameter | Value | Uncertainty (1-sigma) |
| A1 [EST] | 7.447099167683204E-9 | 2.399E-10 |
| A2 [EST] | 8.513230736136108E-11 | 6.346E-11 |
| A3 [EST] | 1.877104598152047E-10 | 6.052E-11 |
|
| | Orbit Determination Parameters
Additional Information
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[ show covariance matrix ]
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