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. 

                                                                                                             (Src : Satellite Comm. – R P khan)

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