This repository provides examples for orbit determination based on laser ranging data, in the form of Jupyter Notebooks.
The open-source orbital dynamics library Orekit (https://www.orekit.org/) is used for all calculations, and in particular the Python wrapper developed by @petrushy: https://gitlab.orekit.org/orekit-labs/python-wrapper
The Orekit example notebooks are based on Orekit 12.1.1 (previously 10.2 IIRC). The Orekit version is frozen in requirements.txt
to avoid breaking changes due to new Orekit major releases.
Create a venv:
python -m venv .venv
Enter the venv:
source .venv/bin/activate
Install the dependencies:
python -m pip install -r requirements.txt
source .venv/bin/activate
jupyter lab
Or just open the notebook in VSCode and select the .venv
as kernel.
The station coordinates files (position&velocity) are updated from time to time. Check out for files named with the format SLRF2020_POS+VEL_xxxxxx.snx
on ftp://cddis.nasa.gov/slr/products/resource/
The newest eccentricities file is always renamed ecc_xyz.snx
and is available at ftp://cddis.gsfc.nasa.gov/slr/slrocc/ecc_xyz.snx