Question: Problem 2 An earth satellite is tracked from ground stations and is observed to have an altitude of 2200 km, a tangential velocity 7 km/s

Problem 2 An earth satellite is tracked from ground stations and is observed to have an altitude of 2200 km, a tangential velocity 7 km/s and a radial velocity of 2.7 km/s. Determine: a) the total orbital energy per unit mass b) the orbital eccentricity e c) the minimum altitude and the maximum speed and d) the true anomalies 0 at the observed position and at the point of maximum speed. e) Identify any potential difficulties with the orbit. 10 mks

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