orbital
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RazerM
High level orbital mechanics package.
From example a code snippet taken- `orbit1 = KeplerianElements.with_period(90 * 60, body=earth) plot(orbit1,title='orbit1') plt.show()` **Showing Error** ** in linspace(*args, **kwargs) [/usr/local/lib/python3.7/dist-packages/numpy/core/function_base.py](https://localhost:8080/#) in linspace(start, stop, num, endpoint, retstep, dtype, axis) 118...
Issues with plotting - doesn't show anything unless plt.show() is called, and orbit rendering issues
It seems that plot/plot2d and plot3d do not display anything, i've tried the following : ``` from numpy import radians from scipy.constants import kilo from orbital import earth, KeplerianElements, Maneuver,...
``` from numpy import array from orbital import elements_from_state_vector r = array([-7.28535000e+07 8.92198056e-09 0.00000000e+00]) v = array([-1.84818933e+00 2.18661193e+03 0.00000000e+00]) mu = 1811405020000000.0 print(elements_from_state_vector(r, v, mu)) ``` prints `OrbitalElements(a=40301757.83775852, e=0.8077004603395054, i=3.141592653589793,...
For Low Earth Orbit inputs of ```python r = np.array([-6478150,0,1200000]) v = np.array([0.0,-7844.111438052,0.0]) ``` The checked calculation in `from_state_vector()` uses these comparisons: ```python abs(out.v - v) # 0.000113, 9.1e-13, 2.1e-5...
I attempted to run the example on the GitHub page. See the attached file. The results I get are Last login: Fri Jan 10 23:56:44 on ttys001 users-MacBook-Pro:~ user$ python...
When trying to plot a 3D graph I am getting the error message 'NameError: name 'plot3d' is not defined' when using code 'plot3d(molniya)' as it is provided in the examples....
Initializing Eutelsat 117 West B from TLE provided in Celestrak for 7/11/2021 I get the error output shown below. I print out the r and v used in `elements.py` for...
I'm running OrbitalPy on a Mac Pro (2019) under Mac OS X Big Sur using the Anaconda distribution Python 3.7. Version 3.3.3 of Matplotlib is used. I get the following...