Table 7
Expected orbital shape of recovered orbit with periapsis altitude of 100 km

Parameters Delta-V margin applied to RM #2 (m/s)
0 100 200
RM #2 Mag. (km/s) 0.207 0.307 0.407
Semi major axis (km) 4,691.369 3,375.134 2,666.888
Eccentricity 0.60399 0.452667 0.30883
Orbital period (hour) 8.041 4.896 3.436
Apoapsis altitude (km) 5,806.739 3,174.269 1,757.776
Altitude at north pole passage (km) 3,463.667 2,209.134 1,348.725
Altitude at south pole passage (km) 348.989 294.132 241.549
Altitude at ascending Node passage (km) 349.931 294.664 241.931
Altitude at descending Node passage (km) 3,458.621 2,207.635 1,348.296
Magnitude of RM #1 is about 0.656 km/s for this case.