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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 2457349.5 (2015-Nov-23.0) TDB
Reference: JPL 84 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | 1.000280111752132 | 1.4549e-06 | |
a | -2938.003982310757 | 15.259 | au |
q | .8229694432560084 | 2.8269e-07 | au |
i | 148.8782970590471 | 8.6312e-06 | deg |
node | 186.1445801306016 | 3.0732e-05 | deg |
peri | 340.3587540701534 | 3.5089e-05 | deg |
M | 4.504628872703906E-5 | 3.5083e-07 | deg |
tp | 2457342.221640340207 (2015-Nov-15.72164034) | 2.0988e-05 | TDB |
period | n/a n/a | n/a n/a | d yr |
n | 6.189071553564886E-6 | 4.8215e-08 | deg/d |
Q | n/a | n/a | au |
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Additional Model Parameters
Parameter | Value | Uncertainty (1-sigma) |
A1 [EST] | 7.573967877099656E-9 | 2.399E-10 |
A2 [EST] | 6.249690700086914E-11 | 6.338E-11 |
A3 [EST] | 1.621151284618413E-10 | 6.054E-11 |
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| | Orbit Determination Parameters
Additional Information
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