A satellite revolves in a circular orbit at a height 200 km from the surface of the earth.If the time period of revolution of satellite is 90 mins,find density of earth if G=6.67*10^-11 Nm^2kg^-2 and radius of earth is 6*10^6 m
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Let the mass of satellite be m and velocity be v.
Distance b/w satellite and center of earth,r=6400+1000=7400
The necessary centripetal force for satellite to revolve around the earth is given by the gravitational attraction b/w earth and satellite
i.e
v=2 *10⁶ ans .....
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