Meysam Mahooti (2023). SGP4 (https://www.mathworks.com/matlabcentral/fileexchange/62013-sgp4), MATLAB Central File Exchange. Retrieved .
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The vectorized SGP4 package was added.
satdata.xndt2o in test_sgp4.m was corrected.
Mjday.m was modified.
test_sgp4.m is modified.
Satellite's state vector is computed in four different coordinate systems, i.e. Earth-centered inertial (ECI), Earth-centered Earth-fixed (ECEF), true of date (TOD) and true equator mean equinox (TEME).