Table 6
Expected orbital shape of recovered orbit with periapsis altitude of 50 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) 4,619.227 3,323.067 2,625.240
Eccentricity 0.60872 0.45919 0.31695
Orbital period (hour) 7.857 4.784 3.356
Apoapsis altitude (km) 5,712.455 3,120.135 1,724.480
Altitude at north pole passage (km) 3,367.221 2,145.563 1,305.910
Altitude at south pole passage (km) 293.561 240.857 190.544
Altitude at ascending Node passage (km) 294.491 241.417 190.975
Altitude at descending Node passage (km) 3,362.506 2,144.041 1,305.238
Magnitude of RM #1 is about 0.655 km/s for this case.