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Study of the Two-Line Element Accuracy by 1U CubeSat with a GPS Receiver

There is a common practice to calculate orbital trajectories of space objects like satellites and space debris using Two-Line Element Sets (TLEs). However, TLEs provide rather coarse parameters for fine orbit computation and their precision varies with age of their issue and position of the satellit...

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Detalles Bibliográficos
Autores principales: Kovář, Pavel, Puričer, Pavel, Kovářová, Kateřina
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9030488/
https://www.ncbi.nlm.nih.gov/pubmed/35458886
http://dx.doi.org/10.3390/s22082902

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