For questions regarding simplified perturbation models and their implementations, regardless of implementation language.
Simplified perturbation 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 in an Earth-centered coordinate frame. The set of models is often referred to collectively as SGP4 due to the prevalence of that algorithm. See the Wikipedia page for more information.
This tag is intended to be used for questions regarding these models and their implementations in any programming language.