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