A satellite is orbiting close to the surface of the earth, then its speed is

\sqrt{2 g R}

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R g

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\sqrt{g R}

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Solution

The correct option is C $\sqrt{g R}$
Speed of satellite orbiting close to earth is given by $v = \sqrt{g R}$

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A satellite is orbiting close to the surface of the earth, then its speed is

The correct option is C √gRSpeed of satellite orbiting close to earth is given by v=√gR

The correct option is C $\sqrt{g R}$
Speed of satellite orbiting close to earth is given by $v = \sqrt{g R}$