(a) Beginning with Eq. (2.3) and Kepler's second law, derive general expressions for vr and vθ for a mass m1 in an elliptical orbit about a second mass m2. Your final answers should be functions of P, e, a, and θ only.
(b) Using the expressions for vr and vθ that you derived in part (a), verify Eq. (2.36) directly from v2=vr2+vθ2.