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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .2397244652494741 | 5.4191e-08 | |
| a | 2.430959697019871 | 1.1834e-08 | au |
| q | 1.848199183608759 | 1.2866e-07 | au |
| i | 6.406709687867922 | 4.1396e-06 | deg |
| node | 256.5106882340106 | 4.8279e-05 | deg |
| peri | 73.60342622845458 | 4.9235e-05 | deg |
| M | 193.3025508861217 | 1.164e-05 | deg |
| tp | 2459641.549429863844
(2022-Mar-03.04942986) | 4.7488e-05 | TDB |
| period | 1384.411075140863
3.79 | 1.0109e-05
2.768e-08 | d
yr |
| n | .2600383704409256 | 1.8989e-09 | deg/d |
| Q | 3.013720210430983 | 1.4671e-08 | au |
|
| | Orbit Determination Parameters
Additional Information
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Physical Parameter Table
| Parameter |
Symbol |
Value |
Units |
Sigma |
Reference |
Notes |
| absolute magnitude |
H |
16.0 |
|
n/a |
MPO449743 |
|
|
| 130006 Imranaslam | Discovered 1999 Nov. 4 by the Catalina Sky Survey. |
| Imran Aslam (b. 1977) is the electronics lead for the OSIRIS-REx Asteroid Sample Return Mission's Laser Altimeter at MDA. Prior to this, he was the Lead for the Mars Curiosity Rover's Alpha Particle X-ray Spectrometer, and Electronics Lead for the Metrology sensors on the Phoenix Mars Lander. |
| 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 2016-11-14 | Last Updated: 2016-11-20 |
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