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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 4 (heliocentric ecliptic J2000)
Element | Value | Uncertainty (1-sigma) | Units |
e | .5690888101335357 | 1.5662e-07 | |
a | 3.384253380113404 | 2.2435e-08 | au |
q | 1.45831265083427 | 5.2702e-07 | au |
i | 21.47906423023408 | 2.7382e-05 | deg |
node | 331.347878452603 | 4.6787e-05 | deg |
peri | 231.1684078259156 | 4.9877e-05 | deg |
M | 187.2366325670216 | 8.6232e-06 | deg |
tp | 2460091.794317219320 (2023-May-27.29431722) | 6.0805e-05 | TDB |
period | 2274.011904470217 6.23 | 2.2612e-05 6.191e-08 | d yr |
n | .1583105168852976 | 1.5742e-09 | deg/d |
Q | 5.310194109392537 | 3.5202e-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 |
16.1 |
|
n/a |
MPO452307 |
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9767 Midsomer Norton (1992 EB1) Discovered 1992-Mar-10 by Steel, D. I. at Siding Spring |
Reference: 19981208/Numbers.arc | Last Updated: 2004-04-19 |
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