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Contents of README:Simplified perturbations models are a set of five mathematical models (SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state vectors of satellites and space debris relative to the Earth-centered inertial coordinate system. This set of models is often referred to collectively as SGP4 due to the frequency of use of that model particularly with two-line element sets produced by NORAD and NASA. |
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Parent Directory - README 16-Dec-2023 03:01 404 sgp4.SlackBuild 16-Dec-2023 03:01 3.2K sgp4.info 16-Dec-2023 03:01 383 slack-desc 16-Dec-2023 03:01 785
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