An earth satellite traveling in the elliptical orbit shown has a velocity as v = 12,149m...

An earth satellite traveling in the elliptical orbit shown has a velocity as v = 12,149mi/hr it passes the end of the semiminor axis at A. The acceleration of the satellite at A is due to gravitational attraction and is 32.23[3959/8400]² = 7.159 ft/sec² directed from A to O. For position A calculate the values of