This contribution contains an algorithm to compute an orbit of a satellite by the third law of Kepler and Newton's law of gravitation. The program loads input data from a file of type two-line elements (TLE).
An input TLE file: https://www.dropbox.com/s/lezxmsxnn6vai5n/TLE_skCUBE.txt?dl=0
This program is a part of a diploma thesis. Author and title of thesis:
Katarína Gombíková: MATLAB for flight engineers (2020).
Peter Szabó and Katarína Gombíková (2019). Keplerian Orbit (https://www.mathworks.com/matlabcentral/fileexchange/72098), MATLAB Central File Exchange. Retrieved July 11, 2019.