A satellite is in an elliptical orbit, with a perigee of 2.0 earth radii and an apogee of 6.6 earth radii. If its velocity is 2.10 km/s at apogee, what is its velocity at perigee?  Provide your answer in km/s.  Hint: Make use of the conservation of angular momentum. A. 6.2 km/s B. 6.9 km/s C. 8.0 km/s D. 8.8 km/s

University Physics Volume 1
18th Edition
ISBN:9781938168277
Author:William Moebs, Samuel J. Ling, Jeff Sanny
Publisher:William Moebs, Samuel J. Ling, Jeff Sanny
Chapter11: Angular Momentum
Section: Chapter Questions
Problem 68P: A satellite in a geosynchronous circular orbit is 42,164.0 km from the center of Earth. A small...
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A satellite is in an elliptical orbit, with a perigee of 2.0 earth radii and an apogee of 6.6 earth radii. If its velocity is 2.10 km/s at apogee, what is its velocity at perigee?  Provide your answer in km/s.  Hint: Make use of the conservation of angular momentum.

A. 6.2 km/s

B. 6.9 km/s

C. 8.0 km/s

D. 8.8 km/s

 

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