CL_op_frozenOrbit — Eccentricity and perigee argument for a frozen orbit
[ecc,pom] = CL_op_frozenOrbit(sma,inc,[,er[,mu[,zonals]]])
Eccentricity and periapsis argument for a frozen orbit can be computed taking into account perturbations coming from terms J2 to Jn of gravitational potential.
You can optionally give the zonals coefficients to be used : default is %CL_j1jn(1:3) (J1/J2/J3). (Please note that if you give %CL_j1jn with n =70, only the first 50 zonals terms will be used, due to algorithm validation).
semi major axis [m] (1x1 : same semi major axis for all inclinations) or (1xM)
inclination [rad] (1x1 : same inclination for all semi major axes) or (1xM)
(optional) equatorial radius [m] (default is %CL_eqRad)
(optional) geocentric gravitational constant [m^3/s^2] (default value is %CL_mu)
(optional) vector of zonals coefficients J1 to Jn (troncated to J50) to be used (default is %CL_j1jn(1:3)) (1 x N)
eccentricity (1xM)
argument of periapsis [rad] (1xM)