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A satellite which is geostationary in a particular is taken to another orbit Its distance from the centre of earth in new orbit is 2 times that of the earlier orbit The time period in the second orbit is
Dear pallavi
we know that when a satellite is revolving around the orbit then relation between time period and radius of orbit is
T2 =(4∏2/GM )a3
where a is radius
(T2/T1)2 =(2a/a)3
T2 = T1√8
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