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A satellite is launched into a circular orbit of radius 'R' around the earth. A second satellite is launched into an orbit of radius 1.03 R. The time period of revolution of the second satellite is larger than the first one approximately by
(3) 4.5%
Kepler: T R3/2 TT= 32 RR
[figure]
RR=3\%
TT=1.5 3\%=4.5\%
Answer: (3)
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