[ hide orbit diagram ]
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .07238289294529401 | 4.075e-08 | |
| a | 2.778612179677235 | 1.6221e-08 | au |
| q | 2.577488191739167 | 1.1432e-07 | au |
| i | 5.471401256769302 | 4.3355e-06 | deg |
| node | 335.2371152564735 | 4.0371e-05 | deg |
| peri | 55.30844590084754 | 4.9287e-05 | deg |
| M | 142.0170193909514 | 2.7262e-05 | deg |
| tp | 2458729.112263213969
(2019-Sep-02.61226321) | 0.00012766 | TDB |
| period | 1691.766143757551
4.63 | 1.4815e-05
4.056e-08 | d
yr |
| n | .2127953685137654 | 1.8634e-09 | deg/d |
| Q | 2.979736167615302 | 1.7395e-08 | au |
|
| | Orbit Determination Parameters
Additional Information
|
[ show covariance matrix ]
Physical Parameter Table
| Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
| absolute magnitude |
H |
15.58 |
|
n/a |
MPCxxxxx |
|
|
| 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 |
|
|
