Hand written solution required

3) (30 pts) An Earth satellite has a semi-major axis of 12,000 km. The orbit eccentricity is 0.3. Find the following: The periapsis and apoapsis radii and velocities b. The specific energy c. The semi-latus rectum and the magnitude of the of the angular momentum d. The radius and velocity magnitudes and flight-path angle for a true anomaly of 1350 and 300 e. Find the maximum flight path angle and the true anomaly at which it occurs (Mathematica might be helpful for this)