Initial Orbit Elements and Orbital Period of a QFLLO
The orbital elements are given in the J2000 frame.
| Orbit | Semi-major axis [km] | Eccentricity | Inclination [deg] | Right ascension of the ascending node [deg] | Argument of perigee [deg] | Mean anomaly [deg] | Orbital period [h] |
|---|---|---|---|---|---|---|---|
| QFLLO | 1937.4 | 0.0005 | 96.8 | 84.8 | 116.2 | 180 | 2.12 |