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  1. Orbital-State-Determination-from-TLE-Data Orbital-State-Determination-from-TLE-Data Public

    This procedure reads Two-Line Element (TLE) orbital data for a geostationary satellite and computes its current position and velocity in Earth-Centered Inertial (ECI) coordinates. This is the found…

  2. LEO-SATELLITE-ORBITAL-STATE-DETERMINATION-PROCEDURE LEO-SATELLITE-ORBITAL-STATE-DETERMINATION-PROCEDURE Public

    This procedure implements the SGP4 (Simplified General Perturbations 4) algorithm for accurately propagating Low Earth Orbit satellite positions. Unlike GEO satellites, LEO satellites experience si…