Pinned Loading
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Orbital-State-Determination-from-TLE-Data
Orbital-State-Determination-from-TLE-Data PublicThis 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…
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LEO-SATELLITE-ORBITAL-STATE-DETERMINATION-PROCEDURE
LEO-SATELLITE-ORBITAL-STATE-DETERMINATION-PROCEDURE PublicThis procedure implements the SGP4 (Simplified General Perturbations 4) algorithm for accurately propagating Low Earth Orbit satellite positions. Unlike GEO satellites, LEO satellites experience si…
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