The Final Project for ASE 366K: Applied Orbital
This is the final project for UT's ASE 366K class. It contains a full fat orbit propagator with algorithms implemented from Vallado version 4.
To run, set your inital conditions in the conds class of the Main file. You will need to know either the inital orbital elements [Semimajor Axis length, eccentrcity, inclination, Right Acension of the Acsending Node, Argument of Periapsis, True Anamoly] or the inital radius and velocity vectors in the J2000 Frame.