Table 4
Best-fit orbital solution (semimajor axis a, perihelion distance q, eccentricity e, inclination i, longitude of ascending node Ω, argument of perihelion ω, mean anomaly M, and perihelion date Tperi), and associated uncertainties, for 2013 AZ60, taken3 from the Minor Planet Center on 2015 March 15.
| a (AU) | 829.7 |
| q (AU) | 7.908098 ± 0.000014 |
| e | 0.990468 ± 0.000010 |
| i (deg) | 16.535760 ± 0.000011 |
| Ω (deg) | 349.21122 ± 0.00002 |
| ω (deg) | 158.14327 ± 0.00021 |
| M (deg) | 0.00876 |
| T peri | 2 456 988.0641 ± 0.0032 |
| Epoch (JD) | 2 457 200.5 |
Notes. The uncertainties of the orbital elements involved throughout the planning of the observations are significantly larger than these due to the shorter arcs available at that time.
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