Inputs are the Keplerian orbital elements, planet properties, and ground station coordinates. Tabs include plots of spacecraft trajectory in the following coordinate systems:
Earth-Centered, Earth-Fixed (Planet-Centered Rotational)
Includes animation and slider controls for plotting the position of the spacecraft within the time frame defined from the time of periapsis passage, tau, to an arbitrary time, t_1. Four example .ini configurations are included to demonstrate usage.
Huy Nguyen (2021). Satellite Trajectory (https://www.mathworks.com/matlabcentral/fileexchange/85273-satellite-trajectory), MATLAB Central File Exchange. Retrieved .
Inspired by: INI Config
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