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The kinetic energy of the satellite in a circular orbit with speed `v` is given as
Options:
(a) `KE =(-GmM_e)/(2(R_e+h))` (b) `KE = (GmM_e)/((R_e+h))`
(c) `KE=(GmM_e)/(2(R_e+h))` (d) `KE = -1/2mv^2`

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