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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…
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sgp4 model models sdp4 space perturbations orbital objects deep orbit nasa simplified sgp sdp8 use km error norad code additional
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| the sun | instance of | and gravitation effects from other bodies | 0.80 | text |
| moon | instance of | and gravitation effects from other bodies | 0.80 | text |
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