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Calculation of Keplerian and Hill's orbital elements for INTELSAT-20 (GEO) and MONILIYA3-50 satellites from position and velocity vectors. Includes orbit visualization and geostationary orbit verification.
This repository contains the integrated Python-STK automated code used to run STK scenarios used in a research project. The research focus was on the 'Orbital Dynamics of In-Orbit Assembly of a Modular Solar Power Satellite in GEO'.