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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