simplifiedPerturbationsModel
Simplified Perturbations Model
https://schema.space/metasat/simplifiedPerturbationsModel
Description: 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 (source)
Example: SGP4
Synonym(s): None
Concept Segments: Space Segment
Concept Families: Orbital Mechanics
Crosswalk Identifiers