Compute the solution of the given problem
Problem- For orbits around the Earth, plot the variation of total energy, maximum kinetic energy, and maximum potential energy as a function of all possible closed orbit eccentricities for a fixed semi-major axis of 25,000km. (μEarth = 398,600.4415 km3/s2, rEarth = 6378 km).
Part 1- What are the minimum and maximum (closed: circular or elliptical) eccentricities for this semi- major axis?
I want experts help to determine the minimum and maximum eccentricities for given semi- major axis.