MATLAB Implementation of Ephemeris Parameters for Satellite Position and Velocity Calculation

Calculating satellite position, velocity, and general orbital parameters using ephemeris data. Provides MATLAB learning materials with practical code implementation examples for satellite trajectory simulation and orbital mechanics algorithms.

Calculating Satellite Velocity in Earth-Centered Earth-Fixed Frame Using 15 Ephemeris Parameters

Computation of satellite velocity and position in Earth-Centered Earth-Fixed (ECEF) coordinates using 15 ephemeris parameters, including 6 Keplerian orbital elements and 9 perturbation parameters