The orbital speed of geostationary satellite is around Options: 3.07 km/s 7.95 km/s 11.2 km/s 15.8 km/s

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A geostationary satellite orbits around the earth in a circular orbit of radius 36,000 km. Then, the time period of a spy satellite orbiting a few hundred km above the earth's surface ( $R_{e}$ = 6400 km) will approximately be

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Q. A geostationary satellite orbits around the earth in a circular orbit of radius

36000 k m

. Then, the period of spy satellite orbiting three hundred kilometers above the earth's surface (

R_{e a r t h} = 6400 k m

) will become :

be:

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