A satellite is orbiting close to the surface of the earth then its speed is
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Let's consider that mass of satellite is m , mass of the the earth is M, radius of the earth is R and acceleration due to gravity is g.
when the satellite is orbiting close to the surface of the earth ,
centripetal force = weight of satellite on earth's surface
or, mv²/R = mg
or, v² = gR
hence, v =
hence, speed of satellite is
when the satellite is orbiting close to the surface of the earth ,
centripetal force = weight of satellite on earth's surface
or, mv²/R = mg
or, v² = gR
hence, v =
hence, speed of satellite is
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