CL_ex_kepler — Keplerian orbit extrapolation
[eph]=CL_ex_kepler(t1,kep,t2[,mu])
Warning when using vectorized calculation: size of kep or size of t2 (M or N) must be 1.
CNES julian day + ut/24 (ut in [h])
keplerian parameters at date t1 [a,e,i,pom,gom,M]' (6xN)
extrapolation date, CNES julian days + ut/24 (ut in [h]) (6xM)
(optional) geocentric gravitational constant. [m^3/s^2] (default value is %CL_mu)
extrapolated ephemerides, date + keplerian parameters [t,a,e,i,pom,gom,M]' (7 x max(N,M))