16. A geostationary satellite is moving in a circular orbit at a height of 36000 km from the surface of
earth. Calculate its speed if it takes 24 hours to revolve around the earth ? (Given radius of earth
= 6400 km)
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The radius of the orbit =6400+36000=42400km
circumference of the orbit 2πR
=2×3.14×42400
=266272km
speed= Time/Distance
=24
266272
=11094.67km/h.
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