Kepler's equation solver by Small Satellites

% Input - Mean anomaly M [rad] , Eccentricity e and Epsilon % Output - eccentric anomaly E [rad] (keplers equation, solver, mean anomaly)

keplerEq(M,e,eps)

Solve Kepler's Equation for E by John Shelton

Calculates Eccentric Anomaly given Mean Anomaly (kepler, aerospace, aerodef)

solve_Kepler_for_E(Me, e, tol)