Hey ppl!<br /><br />Give me the expression for total energy of a orbiting satellite
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23
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★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 :-
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Answered by
1
Hey mate it is
E = GMm/2R
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