Satellite Orbit Simulation
Simulated over a period of 625 days using EGM96 coefficients up to degree 5 and integrated using basic RK4 with a step-size of 30 seconds.
Plotted using Mayavi. Everything was done in Python.
Simulated over a period of 625 days using EGM96 coefficients up to degree 5 and integrated using basic RK4 with a step-size of 30 seconds.
Plotted using Mayavi. Everything was done in Python.