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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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