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2. (50%) At an altitude RA = 4.30 × 106 m above the earth surface, the velocity of the space probe fired from earth has a magnitude of UA-32.5x 106 m/h and an angle of фА-600 with the radial direction. Find (a) the angular momentum per unit mass of the space probe, (b) the θ-component of the velocity, ve, as the probe passes through the point B at the altitude h 12.7 x 106 m above the earth surface. The earth radius is R - 6.37 x 106 m lA = 4.3 Mm R 6370 -12.7 Mm\

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