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A satellite of mass m_s orbits the earth (with mass m_s and radius R_E) with a velocity v and an altitude h. The gravitational force F_G and the centripetal force F_c are given by F_G =Gm_sm_E/(R_E+h)^2, F_c = m_s.v^2/(R_E+h), G= constant a) find the equation of kinetic energy E_ KE(h) of satellite with an altitude (h)

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