CL_kp_M2E — Solution of kepler's equation (ecc,M to E)
E = CL_kp_M2E(ecc,M)
Given the eccentricity ecc and the mean anomaly M, this function computes the eccentric anomaly E
mean anomaly [rad] (1xN)
hyperbolic or elliptical eccentricity (ecc>1) (1xN)
eccentric anomaly [rad] (1xN)
1 CNES - MSLIB FORTRAN 90, Volume V (mvi_kepler_hyperb)
E = CL_kp_M2E(0.001,3*%pi/8)