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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 27 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | .2398918029524855 | 5.1637e-08 | |
| a | 2.430542328521431 | 1.1558e-08 | au |
| q | 1.847475147180093 | 1.2288e-07 | au |
| i | 6.406806957685512 | 4.1175e-06 | deg |
| node | 256.5037044823612 | 4.7909e-05 | deg |
| peri | 73.63892986744945 | 4.8859e-05 | deg |
| M | 245.285431484704 | 1.166e-05 | deg |
| tp | 2459641.531170834036
(2022-Mar-03.03117083) | 4.6644e-05 | TDB |
| period | 1384.054558676934
3.79 | 9.8726e-06
2.703e-08 | d
yr |
| n | .2601053533208522 | 1.8554e-09 | deg/d |
| Q | 3.013609509862769 | 1.4331e-08 | au |
|
| | 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 |
16.11 |
|
n/a |
E2021B55 |
|
|
| 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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