How does the poliastro python package "Going to Mars with Python" example work? What's it really doing?
Why did my vis-viva math solution get so close despite being wrong? Under what conditions would it have been a good approximation?
What formulas do I use to calculate the gravity and drag forces on an object ascending from Earth's surface?
How can I plot satellite's trajectory from three different TLEs to detect any deviation on path with time?
Has Skyfield or any other SGP4-capable open-source Python package yet wrapped/implemented the new, improved SGP4 (version 8+)?
How much delta-v have I used here? What's the "official" equation for delta-v from parametric thrust?
Only top scored, non community-wiki answers of a minimum length are eligible