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.
- Python 3.7+
Create a venv:
python -m venv .venv
Enter the venv:
source .venv/bin/activate
Install the dependencies:
python -m pip install -r requirements.txt
- Enter the venv:
source .venv/bin/activate
- Start Jupyter Lab:
jupyter lab
- Jupyter Lab should pop up in your browser at the URL http://localhost:8888
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