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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 2458080.5 (2017-Nov-23.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | 1.201133796102373 | 2.1064e-05 | |
| a | -1.27234500742808 | 0.00010015 | au |
| q | .2559115812959116 | 6.6635e-06 | au |
| i | 122.7417062847286 | 0.00028826 | deg |
| node | 24.59690955523242 | 0.00025422 | deg |
| peri | 241.8105360304898 | 0.0012495 | deg |
| M | 51.1576197938249 | 0.0061155 | deg |
| tp | 2458006.007321375231 (2017-Sep-09.50732138) | 0.00026424 | JED |
| period | n/a n/a | n/a n/a | d yr |
| n | .6867469493413392 | 8.1084e-05 | deg/d |
| Q | n/a | n/a | au |
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Additional Model Parameters
| Parameter | Value | Uncertainty (1-sigma) |
| A1 [EST] | 2.790193364334668E-7 | 3.574E-8 |
| A2 [EST] | 1.441264159911234E-8 | 2.445E-8 |
| A3 [EST] | 1.57392261588653E-8 | 2.249E-8 |
| ALN [SET] | .0408373333128795 | n/a |
| NK [SET] | 2.6 | n/a |
| NM [SET] | 2. | n/a |
| NN [SET] | 3. | n/a |
| R0 [SET] | 5. | n/a |
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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 |
22.08 |
mag |
.44525 |
2 |
autocmod 2.6k |
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