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

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

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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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Bibliographic Details
Main Authors: Kovář, P. (Author), Kovářová, K. (Author), Puričer, P. (Author)
Format: Article
Language:English
Published: MDPI 2022
Subjects:
Communication satellites
Cubesat
Errors
Geostationary satellites
Global positioning system
GPS-receivers
LEO satellite
LEO satellite orbit
Orbits
Perturbation model
Satellite antennas
Satellite orbit
Satellite position
Simplified perturbation model
simplified perturbations model
Small satellites
Space debris
Tracking (position)
Two line elements
two-line element set
Two-line element sets
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