Prove that at any point on an elliptical orbit, where r = r, v is the velocity,

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Prove that 2 M (7/ - - -) r v = GM at any point on an elliptical orbit, where r = ΙΙrΙΙ, v is the velocity, and a is the semimajor axis of the orbit.

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Calculus

ISBN: 9781319055844

4th Edition

Authors: Jon Rogawski, Colin Adams, Robert Franzosa

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