Use Satellite Communications Toolbox to create a simple satellite scenario from a two-line element (TLE) ephemeris file. Display the orbital elements of all the satellites, including their eccentricity, inclination, right ascension of ascending node, mean anomaly, and period. Show the satellite ground tracks in the Satellite Scenario Viewer, including 20 minutes into the future. Calculate the latitude, longitude, and altitude of one of the satellites at a specific point in time. Add ground stations to the scenario, and calculate the azimuth angle, elevation angle, and range of one of the satellites to one of the ground stations. Play the scenario to show the satellites orbiting the earth.
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