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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 2449246.5 (1993-Sep-16.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .1135945610517189 | 82.516 | |
a | 39.38180490928711 | 3329.4 | au |
q | 34.90824606719221 | 298.53 | au |
i | 2.588781384252404 | 129.74 | deg |
node | 192.0955433319947 | 36.62 | deg |
peri | 180.626895941656 | 2.4869e+05 | deg |
M | .009453345266660303 | 1.967e+05 | deg |
tp | 2449244.129582357932 (1993-Sep-13.62958236) | 4.9322e+07 | TDB |
period | 90269.66931526804 247.14 | 1.1447e+07 3.134e+04 | d yr |
n | .003988050501688392 | 0.50574 | deg/d |
Q | 43.85536375138201 | 3707.7 | 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 |
9.4207 |
|
0. |
3 |
autocmod 2.8 |
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