Path: Orbit/OrbitMechanics
% Time vector for a TLE Time vector for a TLE Type TLETime for a demo. -------------------------------------------------------------------------- Form: t = TLETime( tLE, startDate, endDate, n ) -------------------------------------------------------------------------- ------ Inputs ------ tLE (1,:) TLE string startDate (1,1) or (1,6) Julian date or date array endDate (1,1) or (1,6) Julian date or date array n (1,1) Number of steps (default is 100) ------- Outputs ------- t (1,n) Time vector --------------------------------------------------------------------------