orbital-maneuvers

Calculate time and delta-v requirements for changing orbits within LEO

Installation

Install python 3.11 or greater (3.10 down untested, but may work)
Install packages $ py -m pip install -r requirements.txt

Run

Run get.py with credentials (space-track.org login) to save current debris data
catch.py is the primary calculation script. Ensure your current directory is src when running.
Constants at the bottom of catch.py can be modified
Other files are used to generate graphs