A geostationary satellite is revolving at a height 6R above the earth's surface, where R is the radius of earth. The period of revolution of satellite orbiting at a height 2.5 R above the earth's surface will be:-
24 hours
12 hours
6 hours
6√2 hours
A
24 hours
B
12 hours
C
6 hours
D
6√2 hours
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