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```
>>> from astroquery.jplhorizons import Horizons
>>> obj = Horizons(id='Ceres', location='568',
... epochs={'start':'2010-01-01', 'stop':'2010-03-01',
... …
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It seems impossible to easily deselect an ephemeris marker.
To see what I mean, start on earth and calculate any ephemeris for any body. Now, in the list, select line from the list generated. A ma…
Atque updated
4 years ago
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pour stocker des extensions js pour les callbacks comme `saintsChretiens` et `joursRepublicains`, ou plus tard `rois`
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Hi,
First off, thanks for a really good package! I hope I could contribute something to the project.
However, there's currently an issue I'm having: for only few lines of data from given file I'…
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This will be a nice feature to add as most users won't be bothering about finding the actual velocity and distance metrics. Hope we can get that from here?
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Good morning,
I am using as a baseline the Single Perturbed Satellite Propagator example, with few changes: I changed the reference frame from J2000 to ECLIPJ2000 (changing also the initial condition…
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Satellites
GPS
Low, medium, high
by company
Lagrange points
* moon
* sun
https://bl.ocks.org/vasturiano/818f5fa0f91f9f3d8a29efe9bf66f8b3
https://nbremer.github.io/planet-globe/
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**Is your feature request related to a problem? Please describe.**
There is currently no way to compute the ephemerides for several days with Kosmorro.
**Describe the solution you'd like**
New ar…
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Hello,
I am trying to run a Monte Carlo simulation of `SingleSatellitePropagator`. I modified the code a little to run a completely independent computation for different initial conditions of posit…
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### Description
Please could you implement the true equator mean equinox transform? SGP4 satellite position-velocity
ephemerides are produced in the TEME frame. For the majority, …
c3-14 updated
4 years ago