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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .1532140240034486 | 3.8082e-08 | |
a | 2.665921592964087 | 1.3117e-08 | au |
q | 2.257465018028376 | 1.0487e-07 | au |
i | 13.68418114883726 | 4.7717e-06 | deg |
node | 161.8438288083912 | 1.6515e-05 | deg |
peri | 95.64549781315711 | 2.3349e-05 | deg |
M | 310.543740203885 | 1.6892e-05 | deg |
tp | 2459218.917913284746 (2021-Jan-04.41791328) | 7.5162e-05 | TDB |
period | 1589.898813753107 4.35 | 1.1734e-05 3.213e-08 | d yr |
n | .226429504120571 | 1.6711e-09 | deg/d |
Q | 3.074378167899799 | 1.5127e-08 | au |
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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 |
14.9 |
|
n/a |
MPO432203 |
|
rotation period |
rot_per |
7.47 |
h |
n/a |
LCDB (Rev. 2020-October); Warner et al., 2009 |
Result based on less than full coverage, so that the period may be wrong by 30 percent or so. Published Reference List: [Erasmus, N.; McNeill, A.; Mommert, N.; Trilling, D.E.; et al. (2019) Ap. J. Suppl. Series 242, A15.] |
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65113 (2002 CD47) Discovered 2002-Feb-03 by NEAT at Haleakala |
Reference: 20030614/Numbers.arc | Last Updated: 2004-04-19 |
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