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If a geostationary satellite is orbiting the earth at a height of 6R above the surface of the Earth R being the radius of the Earth then what will be the

time period of another satellite of height 2.5R from the surface of the earth?



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and for geostationary satellite T = 24 hr
 so T2 = 24/2√2 = 6√2 hr
2 4 2
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