(a) Â the total energy of the satellite when it is at A:-
   E = PE + KE = - G*Me*M/a + 1/2mv₀²
(b) the magnitude of the angular momentum of the satellite about the center of the Earth when it is at A:-
  L = mvr = mv₀a
(c) Conservation of angular momentum gives, Â
  mv₀a =  mvᵇb, or vᵇ = v₀a/b
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