Скачать или смотреть Plot Keplerian / Classical Orbital Elements | Orbital Mechanics with Python 10

In this video I go over how to make a plotting function for the keplerian orbital elements over time after orbit propagation. I show how I implemented a 2 rows by 3 columns subplot to include all COEs in one figure. I then implement an example with the ISS orbit and how the keplerian orbital elements change due to the J2 perturbation.

Pre-req videos:
1. Introduction / Overview -    • Introduction to Orbital Mechanics with Pyt...  
4. Developing the OrbitPropagator Class and the Planetary Data File -    • OrbitPropagator Class and Planetary Data F...  
5. tools.py and the plot_n_orbits() function -    • Tools file and the plot_n_orbits() Functio...  
6. Keplerian Orbital Elements -    • Keplerian / Classical Orbital Elements | O...  
8. J2 Perturbation -    • J2 Perturbation | Orbital Mechanics with P...  
9. rv2coes() Function -    • Convert State Vector to Keplerian Orbital ...  

Optional videos:
2. Two Body Problem / ODE Solvers -    • The Two Body Problem / ODE Solvers | Orbit...  
3. Developing the 3D Plotting Function -    • Developing the 3D Plotting Function | Orbi...  

Link to matplotlib documentation:
https://matplotlib.org/