Optimum method presented makes use of orbit inclination and elements in plane, and proceeds with differential correction of orbit elements; accuracy of method is compared with purely geometrical, and least-squares geometrical method.


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    Title :

    Determination of satellite orbits from radar data


    Additional title:

    NASA -- Tech Note


    Contributors:
    Cahill, W.F. (author) / Harris, I. (author)


    Publication date :

    1960


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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