The early-orbit capability of the Goddard Trajectory Determination System, which determines starting vectors for earth satellites from angles-only or range-angles observations, is described and documented. Early-orbit results obtained from a variety of satellites, data types and methods of solution are also presented.


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    Title :

    GPS early-orbit subsystem for earth satellites


    Contributors:
    Laczo, V. T. (author) / Maury, J. L. (author)

    Publication date :

    1972-12-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English


    Keywords :


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