Table 1
Summary of the orbital characteristics for the two orbit recovery cases

Recovered orbit’s characteristics	Recovery Option Case 1	Recovery Option Case 2
Orbital shape	Circular mission orbit	Elliptical mission orbit
Considered periapsis altitude (km)	30, 50, 100, 200, 500, and 1,000	30, 50, and 100
Semi-major axis	Computed using periapsis altitude	Computed using available RM2 magnitude with consideration of periapsis altitude
Eccentricity	0	↑
Inclination (°)	90	←
Right Ascension of Ascending Node (°)	0	←
Argument of Periapsis (°)	0	45 (re-oriented)
True Anomaly (°)	0	←