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Hi! Thanks for the wonderful package. I'm using the DE440 kernels, and trying to get the osculating elements. It seems like the `data.gravitational_parameters.GM_dict` is missing a `0` key for the SSB…
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**Is your feature request related to a problem? Please describe.**
Often for mission planning, the TLE is needed. Need something that can generate TLEs from user-supplied keywords and vice-versa. K…
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Submit your add-ons in this issue, thanks for your contribution!
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**Describe the bug**
Hi, amazing package and congratulations on the recent publication 🎉
I just had a quick orbital elements issue in `KeplerianOrbit` that I am running into. It was my understandi…
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Hi. I used an example from the SatelliteToolbox.jl‘s [document](https://juliaspace.github.io/SatelliteToolbox.jl/dev/man/orbit/propagators/#Examples).
```julia
orbp = init_orbit_propagator(Val(:tw…
ZMAlt updated
3 years ago
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Would it be possible to add functions that return "processing" time and "fixed processing" time, which would return the value you would get (in principle, ignoring precision issues) if you added proce…
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I am trying to compare various `poliastro` orbit propagation methods vs the `spg4` propagator. However, the resulting state vectors are significantly different between both.
🐞 **Problem**
Essent…
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Current Pluto trail is very short. There is much desire to be able to see more of the Pluto's trail. We have discussed offering a Kepleraian version of the trail as well, but I found not mention of th…
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pytest is ok ,but when I run main.py An error was found, but returning just with the version: No module named 'termios'
C:\Users\astronomy\PycharmProjects\untitled1\orbitdeterminator\orbitdete…
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Is it possible to add keplerian element result for Initial Orbit Determination (IOD) module?
Now, there is only the velocity solution of Lambert problem.
I think since it is orbit determination, kep…