The period of revolution of an earth's satellite close to the surface of earth is 90 minutes. The period of another earth's satellite in an orbit at a distance of three times earth's radius from its surface will be
A
90 minutes
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B
90×√8 minutes
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C
270 minutes
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D
720 minutes
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Solution
The correct option is C 720 minutes Time period, T2=4π2GMR3 i.e T2∝R3 ⇒(T1T2)2=(R1R2)3
Here, R1=Re and R2=Re+3Re=4Re ∴(T1T2)2=(Re4Re)3 ⇒902T22=164