How to Install and Uninstall python3-sgp4.x86_64 Package on Fedora 39
Last updated: November 25,2024
1. Install "python3-sgp4.x86_64" package
Here is a brief guide to show you how to install python3-sgp4.x86_64 on Fedora 39
$
sudo dnf update
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$
sudo dnf install
python3-sgp4.x86_64
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2. Uninstall "python3-sgp4.x86_64" package
Please follow the guidelines below to uninstall python3-sgp4.x86_64 on Fedora 39:
$
sudo dnf remove
python3-sgp4.x86_64
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$
sudo dnf autoremove
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3. Information about the python3-sgp4.x86_64 package on Fedora 39
Last metadata expiration check: 2:03:11 ago on Thu Mar 7 17:44:52 2024.
Available Packages
Name : python3-sgp4
Version : 2.23
Release : 1.fc39
Architecture : x86_64
Size : 211 k
Source : python-sgp4-2.23-1.fc39.src.rpm
Repository : updates
Summary : Compute position and velocity of earth-orbiting satellites
URL : https://pypi.python.org/pypi/sgp4
License : MIT AND SGP4
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.
Available Packages
Name : python3-sgp4
Version : 2.23
Release : 1.fc39
Architecture : x86_64
Size : 211 k
Source : python-sgp4-2.23-1.fc39.src.rpm
Repository : updates
Summary : Compute position and velocity of earth-orbiting satellites
URL : https://pypi.python.org/pypi/sgp4
License : MIT AND SGP4
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.