Abstract The large elliptical orbit is a large-eccentricity orbit with the apogee altitude several times higher than the earth’s radius. Because of its orbital characteristics, the satellite has a slow operating velocity and long duration on the side of the apogee. With wide coverage area, it can complete various space and earth observation missions.


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    Title :

    Orbit Design of Spacecraft on Elliptical Orbit


    Contributors:
    Liu, Fucheng (author) / Lu, Shan (author) / Sun, Yue (author)


    Publication date :

    2018-08-15


    Size :

    45 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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