Converting a state vector/orbital elements to a TLE

Version 1.0.1 (323 ko) par David Eagle
MATLAB scripts that can be used to calculate an a Two Line Element (TLE) from a user-provided osculating state vector or orbital elements.
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Mise à jour 28 déc. 2022

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MATLAB script that can be used to calculate an approximate Two Line Element (TLE) set from a user-provided osculating state vector or classical orbital elements. It is valid for spacecraft that can be modeled using the NORAD SGP4 algorithm. Includes PDF users guide.

Citation pour cette source

David Eagle (2024). Converting a state vector/orbital elements to a TLE (https://www.mathworks.com/matlabcentral/fileexchange/104065-converting-a-state-vector-orbital-elements-to-a-tle), MATLAB Central File Exchange. Récupéré le .

Compatibilité avec les versions de MATLAB
Créé avec R2019b
Compatible avec toutes les versions
Plateformes compatibles
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Version Publié le Notes de version
1.0.1

Added Scott Campbell's algorithm
1.0.0