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.
This requires: serialDV
Maintained by: Andrea Sacchetti Picchio
Keywords: satellite,library
ChangeLog: sgp4
Homepage:
https://github.com/dnwrnr/sgp4/
Download SlackBuild:
sgp4.tar.gz
sgp4.tar.gz.asc (FAQ)
(the SlackBuild does not include the source)
Individual Files: |
README |
sgp4.SlackBuild |
sgp4.info |
slack-desc |
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