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Question
An artificial satellite moving in a circular orbit around the earth has a total (kinetic + potential) energy E0. Its potential energy is
Options:
A .  −E0
B .  1.5E0
C .  2E0
D .  E0
Answer: Option C
:
C
Potential energy = 2×(Totalenergy)=2E0
Because we know = U=GMmrandE0=GMm2r

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