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For a satellite moving in an orbit aroun the earth the ratio of kinetic enrgy and potential enrgy is :A. ` - 1/2`B. ` 2`C. ` sqrt 2`D. ` 1/(sqrt2`

Answer» Correct Answer - A
`K.E. = + 1/2 e^2 /r-n and p.E. =- e^2/r_n`.


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