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Table 4
1-sigma standard deviations of the orbital elements of the orbits of 2008 YB3 and 2005 VD, used to define the orbital elements of the orbits of the clones.
Orbital element (unit) | 2008 YB3 | 2005 VD |
|
||
Semimajor axis (AU) | 0.000471 | 0.001605 |
Eccentricity | 0.00002077 | 0.0001479 |
Inclination (°) | 0.0000549 | 0.0003509 |
Longitude of Node (°) | 0.0001475 | 0 .003448 |
Argument of perihelion (°) | 0.002243 | 0.03649 |
Mean Anomaly (°) | 0.0008794 | 0.01661 |
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