Class 11th !
Derive an expression for orbital velocity of satellite .
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Explanation:
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Total Energy of a Satellite
★The total energy is obtained by adding the expressions of kinetic and potential energy :-
→ E = P.E + K.E
= - GMm/(R+h) + ½mv² = -GMm/2 ( R + h )
But when a Satellite is orbiting close to the surface of earth , r ≈ R
In this case - total energy is given by :-
E = -GMm/2R
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