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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .0722247045519212 | 4.0847e-08 | |
| a | 2.778941119695956 | 1.6242e-08 | au |
| q | 2.57823291835873 | 1.1468e-07 | au |
| i | 5.471190852070882 | 4.3356e-06 | deg |
| node | 335.2371645495092 | 4.0588e-05 | deg |
| peri | 55.34636766605652 | 4.9551e-05 | deg |
| M | 100.2869544598823 | 2.7341e-05 | deg |
| tp | 2458729.132770204698
(2019-Sep-02.63277020) | 0.00012823 | TDB |
| period | 1692.066566785521
4.63 | 1.4834e-05
4.061e-08 | d
yr |
| n | .2127575871225355 | 1.8652e-09 | deg/d |
| Q | 2.979649321033181 | 1.7415e-08 | au |
|
| | Orbit Determination Parameters
Additional Information
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Physical Parameter Table
| Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
| absolute magnitude |
H |
15.5 |
|
n/a |
MPO502795 |
|
|
| 118769 Olivas | Discovered 2000 Aug. 28 by M. W. Buie at Cerro Tololo. |
| John D. Olivas (b. 1966) is a former American astronaut. Olivas flew two Space Shuttle missions to assemble the International Space Station (in 2007 and 2009). He conducted five space walks during those two missions. |
| NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character) |
| Reference: MPC batch dated 2021-01-27 | Last Updated: 2021-02-23 |
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