MATLAB Code Implementation for Satellite Orbit Visualization

MATLAB code provides an effective solution for visualizing satellite orbits, which serves as a valuable tool for understanding satellite motion dynamics. The implementation typically involves calculating orbital parameters using Keplerian elements and transforming them into 3D Cartesian coordinates through coordinate system conversions. The visualization covers 6 satellite orbital planes, each characterized by unique inclination angles, altitudes, and specific operational purposes. Key implementation aspects include utilizing MATLAB's 3D plotting functions like plot3() or scatter3() to render orbital trajectories, while employing transformation matrices for accurate spatial positioning. The code may incorporate time-dependent position calculations using orbital mechanics equations to predict satellite locations, which is crucial for satellite communication planning and scientific research applications. Learning this implementation technique enhances comprehension of orbital mechanics while providing practical skills for aerospace engineering, telecommunications, and research projects. The methodology involves defining orbital parameters (semi-major axis, eccentricity, inclination), implementing coordinate transformations between Earth-Centered Inertial (ECI) and Earth-Centered Earth-Fixed (ECEF) frames, and creating animated visualizations using MATLAB's handle graphics system.