Determine the apparent velocity v rel of a satellite moving in a circular equatorial orbit 200 mi

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Determine the apparent velocity vrel of a satellite moving in a circular equatorial orbit 200 mi above the earth as measured by an observer on the equator 

(a) For a west-to-east orbit 

(b) For an east-to-west orbit. Why is the west-to-east orbit more easily achieved?

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Engineering Mechanics Dynamics

ISBN: 9781118885840

8th Edition

Authors: James L. Meriam, L. G. Kraige, J. N. Bolton

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