Question

A satellite which is geostationary in a particular

orbit 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​

Answer 1

Answer:

First time T^2×R^3

Second time T^2×(2R) ^3

T1/T=(2R) ^3/(R) ^3/2=(2) ^3/2

T1 =2^3/2T (T =24 hour for geostationary satellite)

T=,2√2×24= 48√2

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