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Quiz - Satellite Orbital Parameters
Satellite Communications, Keplers Laws, Orbital Mechanics
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Division
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Roll No.
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Orbit has eccentricity of 0.15 and semi major axis of 9000km. Determine Periodic time and Apogee height
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Periodic Time
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Apogee height
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For a satellite perigee & apogee height is 300km and 42000km resp. Find velocities at apogee & perigee by assuming earth radius 6378km.
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Apogee Velocity
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Perigee Velocity
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Sum & difference of apogee and perigee distances are 50000km & 30000km for a certain elliptical satellite orbit. Determine eccentricity.
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eccentricity
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If apogee height and perigee height is of 39342km & 613km. Determine semi major axis & eccentricity.
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semi major axis
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eccentricity
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