The time period of a satellite in a circular orbit of radius R is T. The period of another satellite in a circular orbit of radius 4R is?
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from ceplar we know that
T^2 directly proportional to R^3
Now taking ratio the directly proportional sign as well as constant part removed
(T1/T2)^2 = (R/4R)^3
(T1/T2)^2= 1/64
T1/T2 = 1/8
T2/T1= 8
T2 = 8T1
hope help you :-)
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