Open Access

Table A.1

Orbital elements at epoch 2015 July 3, 12:49:34.597424 TDT.

Seven-parameter solution
Semi-major axis (a) 1.312379822554 ± 9.56 × 10−10 au
Eccentricity (e) 0.21469485268 ± 9.80 × 10−9
Inclination (i) 2.21285565 ± 1.28 × 10−6 deg
Longitude of ascending node (Ω) 71.0863668 ± 2.97 × 10−5 deg
Argument of perihelion (ω) 298.7958058 ± 3.43 × 10−5 deg
Mean anomaly (m) 179.09376684 ± 7.13 × 10−6 deg
A2 (−2.135 ± 0.300) × 10−14 au/day2
χ2 0.446

Notes. The angles refer to the J2000 ecliptic frame. The reported uncertainties correspond to the 1-σ level. χ2 denotes the RMS of the normalised post-fit residuals.

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