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author | Sharlatan Hellseher <sharlatanus@gmail.com> | 2022-11-28 23:27:18 +0000 |
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committer | Ludovic Courtès <ludo@gnu.org> | 2022-12-05 22:22:20 +0100 |
commit | 7f380a2e26f59ef99b4a02d65c67192a9ad24cb5 (patch) | |
tree | 0e2790cf0b876760e5b991a6d3295bcc889cb590 /gnu/packages/astronomy.scm | |
parent | 6468d9c131921c82a4389f0c1670807fb635f4f2 (diff) | |
download | guix-7f380a2e26f59ef99b4a02d65c67192a9ad24cb5.tar.gz |
gnu: python-sgp4: Move to astronomy.
* gnu/packages/astronomy.scm: (python-sgp4): Move here from python-science.scm. [description]: Expand description, annotate acronyms, add link to CelesTrak. Signed-off-by: Ludovic Courtès <ludo@gnu.org>
Diffstat (limited to 'gnu/packages/astronomy.scm')
-rw-r--r-- | gnu/packages/astronomy.scm | 29 |
1 files changed, 29 insertions, 0 deletions
diff --git a/gnu/packages/astronomy.scm b/gnu/packages/astronomy.scm index 759ccbec9e..d4c886e82b 100644 --- a/gnu/packages/astronomy.scm +++ b/gnu/packages/astronomy.scm @@ -1464,6 +1464,35 @@ re-gridding of images from one world coordinate system to another e.g. changing the pixel resolution, orientation, coordinate system.") (license license:bsd-3))) +(define-public python-sgp4 + (package + (name "python-sgp4") + (version "2.21") + (source + (origin + (method url-fetch) + (uri (pypi-uri "sgp4" version)) + (sha256 + (base32 "1vzcrlrlzmhbycdz16m8v241l8zx49vsy81wcd0yjxs80isvhyb1")))) + (build-system python-build-system) + (propagated-inputs + (list python-numpy)) + (home-page "https://github.com/brandon-rhodes/python-sgp4") + (synopsis "Track earth satellite TLE orbits using SGP4") + (description + "This package provides a Python implementation for computations of the +position and velocity of an earth-orbiting satellite, given the satellite’s +@acronym{TLE, Two-line element set} orbital elements from a source like +@url{CelesTrak, https://celestrak.org/}. + +It implements the most recent version of @acronym{SGP4, Simplified General +Perturbation models}, and is regularly run against the SGP4 test suite to make +sure that its satellite position predictions agree to within 0.1 mm with the +predictions of the standard distribution of the algorithm. This error is far +less than the 1–3 km/day by which satellites themselves deviate from the ideal +orbits described in TLE files.") + (license license:expat))) + (define-public python-sunpy (package (name "python-sunpy") |