Table 5
Expected orbital shape of recovered orbit with periapsis altitude of 30 km

Parameters Delta-V margin applied to RM #2 (m/s)
0 100 200
RM #2 Mag. (km/s) 0.208 0.308 0.408
Semi major axis (km) 4,590.443 3,302.130 2,608.488
Eccentricity 0.61064 0.46184 0.32024
Orbital period (hour) 7.783 4.738 3.324
Apoapsis altitude (km) 5,674.488 3,098.261 1,710.976
Altitude at north pole passage (km) 3,328.709 2,119.888 1,288.517
Altitude at south pole passage (km) 271.4732 219.5140 170.1137
Altitude at ascending Node passage (km) 272.4051 220.0940 170.5752
Altitude at descending Node passage (km) 3,323.912 2,118.365 1,287.837
Magnitude of RM #1 is about 0.655 km/s for this case.