Find maximum eccentricities for given semi-major axis

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Reference no: EM13719677

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.

Reference no: EM13719677

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