A satellite in a circular orbit of radius R has a period of 4 hours. Another satellite with orbital radius 3R around the same planet will have a period of (in hours):
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Using Kepler's 3rd law of planetary motion we have, R 3 T 2 = constant Thus, R 3 4 2 = ( 3 R ) 3 T 2 or, T = 4 2 7 .