Table B.1
Orbital elements of 252P and BA14 and their 1σ uncertainties at Epoch 2 457 519.5 (=2016 May 11.0).
| Object | a(a) | e(b) | i(c) | ω (d) | Ω (e) | M (f) |
|---|---|---|---|---|---|---|
| 252P | 3.0470 | 0.6731 | 10.4223 | 343.3110 | 190.9499 | 10.5137 |
| (6.3018 × 10-5) | (6.8756 × 10-6) | (6.3172 × 10-5) | (5.4848 × 10-5) | (6.2681 × 10-5) | (3.000 × 10-4) | |
| BA14 | 3.0216 | 0.6662 | 18.9181 | 351.9022 | 180.5312 | 40.8120 |
| (8.4014 × 10-7) | (9.2653 × 10-8) | (1.7085 × 10-6) | (4.5491 × 10-6) | (2.209 × 10-6) | (1.7161 × 10-5) | |
Notes. (a) The semimajor axis in au; (b)the eccentricity; (c) the inclination in degrees; (d) the argument of perihelion in degrees; (e) the longitude of the ascending node in degrees; and (f)the mean anomaly in degrees. Numbers in parentheses are 1σ uncertainties of the orbital elements. All the values are quoted from the JPL Small-Body Database Browser (https://ssd.jpl.nasa.gov/sbdb.cgi).
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