Our goal is to determine the best orbit that will allow a ground station (so this is a fixed point on earth) to communicate a maximum number of times par day with a LEO satellite.
So the question is : Is there mathematical models/equations used to determine the optimal orbit for a LEO satellite that will allow us to communicate a maximum number of times per day with a certain point on Earth ?
PS : We already used STK to test some arbitrary orbits and calculate the number of times the satellite entred in communication with the ground station (and thus the total communication time), but we want a more "scientific" method.