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Table 2
Orbital elements at epoch 2016 December 30 11:22:22.2765 TDT.
Six-parameter solution | |
---|---|
Semi-major axis (a) | 1.00110467203 ± 2.00 × 10−9 au |
Eccentricity (e) | 0.104039114 ± 1.42 × 10−7 |
Inclination (i) | 7.77268000 ± 1.02 × 10−5 deg |
Longitude of ascending node (Ω) | 66.4731422 ± 1.26 × 10−5 deg |
Argument of perihelion (ω) | 307.1331147 ± 1.92 × 10−5 deg |
Mean anomaly (m) | 87.6602276 ± 2.92 × 10−5 deg |
χ2 | 0.415 |
Seven-parameter solution | |
---|---|
Semi-major axis (a) | 1.00110464825 ± 7.30 × 10−9 au |
Eccentricity (e) | 0.104037949 ± 3.84 × 10−7 |
Inclination (i) | 7.7725957 ± 2.77 × 10−5 deg |
Longitude of ascending node (Ω) | 66.4732214 ± 2.71 × 10−5 deg |
Argument of perihelion (ω) | 307.133111 ± 1.92 × 10−5 deg |
Mean anomaly (m) | 87.6601337 ± 4.06 × 10−5 deg |
A2 | (−1.434 ± 0.410) × 10−13 au day−2 |
χ2 | 0.403 |
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