Introduction to Orbit Propagation and Visualization
Use Aerospace Toolbox or Satellite Communications Toolbox to create a simple satellite scenario from a two-line element (TLE) set. 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.
选择中国网站（中文或英文）以获得最佳网站性能。其他 MathWorks 国家/地区网站并未针对您所在位置的访问进行优化。