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I've just started to study skyfield, but I'd like to use it in a project where propagate satellite vectors numerically but I would like to return them to EarthSatellite to make use of the Topos and ot…
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Hi, I was just thinking that, for the benefit of those new to astronomy and satellites (like myself), it might be useful to mention somewhere in the documentation some of the nuances around what SGP4 …
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I think this is a clarification request relating to the API webpages.
Is it possible to use Skyfield to propagate a TLE forwards and then output an element set, rather than the geometric x,y,z ? I'd …
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Hi Everyone
My computer crashed a few days ago and I had to reinitialise everything.
I am trying to resent tudat on my virtual environment `astrodynamic_venv` but I am having the following error w…
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It seems that `pykep.ic2par` returns the mean anomaly instead of the eccentric one:
```Python
import pykep
r=(-1322756.9200525356, -3353314.2849302134, 6087211.963478714)
v=(-127.4601321873357, …
Sceki updated
2 years ago
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Reasons why I think YAML configs are good:
1) Plain text configs sometimes hard to read because different options are mixed together. For example
```
KEP ! Use Kepleria…
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Hi all,
To preface: this is probably not an issue with REBOUND, and almost certainly is just a silly mistake on my end. But I can't find it, so any help would still be appreciated.
I've been ex…
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I am trying to setup a J2 propagator using the following modules:
```
from poliastro.twobody import orbit
from poliastro import constants
from poliastro.bodies import Earth
from poliastro.core.…
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tldr; I find that I receive different Keplerian orbital elements when calculating them in post versus printing them as a REBOUND simulation is running.
I have run a simulation of the full solar sys…
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# Feature
## Desired behavior
Same # of conjunction
## What needs to be done
Run with different dt in cfg
## How it can be tested
Run