Satellite Orbital Mechanics
Satellite Orbital Mechanics
Quiz
Q.1) Orbit has eccentricity of 0.15 and semi major axis
of 9000 km. Determine Periodic time and Apogee height.
Q.2) For a satellite perigee & apogee height is 300 km
and 42000 km respectively. Find velocities at apogee & perigee by assuming earth
radius 6378 km.
Q.3) Sum & difference of apogee and perigee distances
are 50000 km & 30000 km for a certain elliptical satellite orbit. Determine
eccentricity.
Q.4) If apogee height and perigee height is of 39342 km
& 613 km. Determine semi major axis & eccentricity.
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