Given that a satellite has to be shifted 300km further from Earth than it's original geosynchronous orbit (that has period = 24hrs & radial distance of 42300km from center of the planet). Using most of the derivations from Newton's 2nd Law, a. what is the orbital period of the new orbit after shifting in hrs? b. How much energy would it take to move to new orbit if mass of satellite = 6350kg ? Givens -> Mass of earth = 5.98x10^24 kg G= 6.673x10^-11 (you can use other constants)

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