A satellite has the following orbital characteristics:
T = 42164 seconds (orbital period)
e = 0.6 (eccentricity)
ω = 90° (argument of perigee)
i = 55° (inclination)
Ω = 60° (right ascension of the ascending node)
tp = 0 ( time of perigee passage)
a). Determine the altitude when the satellite crosses the equator.
b). Determine the minimum and maximum altitudes of the satellite and the latitudes at which they occur.
c). Determine the amount of time in a single orbital revolution that the satellite is in the Northern Hemisphere.