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12 Jan 2013 Optimal Impulsive Orbital Transfer MATLAB script for the solution of the one and two impulse orbit transfer between two Earth orbits. Author: David Eagle

Yes. Hohmann only describes a transfer between two coplaner circular orbits. This specifically solves the more general problem of minimizing the delta-v between orbits with eccentricities less than 1 (general elliptical problem that includes circular) that might have an inclination difference between them or even be on a different ascending node. The minimum solution will split inclination change in between the two burns.

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