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