https://bugzilla.redhat.com/show_bug.cgi?id=2156932
Bug ID: 2156932
Summary: Review Request: python-sgp4 - Compute position and
velocity of earth-orbiting satellites
Product: Fedora
Version: rawhide
Hardware: All
OS: Linux
Status: NEW
Component: Package Review
Severity: medium
Priority: medium
Assignee: [email protected]
Reporter: [email protected]
QA Contact: [email protected]
CC: [email protected]
Target Milestone: ---
Classification: Fedora
Spec URL: https://mattia.fedorapeople.org/python-sgp4/python-sgp4.spec
SRPM URL:
https://mattia.fedorapeople.org/python-sgp4/python-sgp4-2.21-1.fc38.src.rpm
Description: This Python package computes the position and velocity of an
earth-orbiting
satellite, given the satellite’s TLE orbital elements from a source like
CelesTrak. It implements the most recent version of SGP4, 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.
Fedora Account System Username: mattia
COPR scratch build with example review:
https://copr.fedorainfracloud.org/coprs/mattia/Testing/build/5188372/
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