The orbit of a geostationary satellite is concentric and coplanar with the equator of the earth and rotates along the direction of rotation of earth calculate height and speed given mass of earth =5.98×10^27, radius =6400km, π^2=9.87 , g =9.81
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When a satellite travels in a geosynchronous orbit around the Earth, it needs to travel at a certain orbiting radius and period to maintain this orbit.
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