Answer in python

ponts "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy namely Rath E = u? + |.ng'.. dRg", Ro Ryth where Ro is the radius of the Earth and h is the where g 9.8 is the acceleration due to gravity and u, is the satellite velocity usRo height above the Earth at which the satellite orbits. Roth What is the energy E necessary to put a satellite into orbit at h 10 x 10 m, in units of J? Work in SI to obviate the need for a unit system in this problem. Store your result in a variable energy, which should be a sympy expression. You should also include an intermediate variable us, which should also be a sympy expression. . Use the symbolic variable Re instead of R e to be consistent with the autograder. This exercise (and the quote) is derived from Sutton & Biblarz, _Rocket Propulsion Elements, p. 120 ponts "The energy E necessary to bring a unit of mass into a circular satellite orbit neglecting drag, consists of kinetic and potential energy namely Rath E = u? + |.ng'.. dRg", Ro Ryth where Ro is the radius of the Earth and h is the where g 9.8 is the acceleration due to gravity and u, is the satellite velocity usRo height above the Earth at which the satellite orbits. Roth What is the energy E necessary to put a satellite into orbit at h 10 x 10 m, in units of J? Work in SI to obviate the need for a unit system in this problem. Store your result in a variable energy, which should be a sympy expression. You should also include an intermediate variable us, which should also be a sympy expression. . Use the symbolic variable Re instead of R e to be consistent with the autograder. This exercise (and the quote) is derived from Sutton & Biblarz, _Rocket Propulsion Elements, p. 120