How to Install and Uninstall python3-sgp4 Package on Ubuntu 21.10 (Impish Indri)

Last updated: November 26,2024

1. Install "python3-sgp4" package

This is a short guide on how to install python3-sgp4 on Ubuntu 21.10 (Impish Indri)


    
        
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                sudo apt update
            
                    
    
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                sudo apt install
            
                        
                python3-sgp4
            
                    
    
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2. Uninstall "python3-sgp4" package

Please follow the instructions below to uninstall python3-sgp4 on Ubuntu 21.10 (Impish Indri):


    
        
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                sudo apt remove
            
                        
                python3-sgp4
            
                    
    
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                sudo apt autoclean && sudo apt autoremove
            
                    
    
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3. Information about the python3-sgp4 package on Ubuntu 21.10 (Impish Indri)

Package: python3-sgp4
Architecture: amd64
Version: 2.15-0.1
Priority: optional
Section: universe/python
Source: sgp4
Origin: Ubuntu
Maintainer: Ubuntu Developers
Original-Maintainer: Ulises Vitulli
Bugs: https://bugs.launchpad.net/ubuntu/+filebug
Installed-Size: 367
Depends: python3:any
Filename: pool/universe/s/sgp4/python3-sgp4_2.15-0.1_amd64.deb
Size: 92872
MD5sum: 2ccdeb0bfcc7558eaa41395f8d38440f
SHA1: 827dc7ecdd0218b358a303f03b3b82c4af57da3d
SHA256: 6f9a9a2ddd5931d57ffec0e684eded6a4a21cf185f2dd69acecd86c548384d34
SHA512: afe683f600eeb4695210f45ac6a84faffaab2ae4a3fbae05764022c6bc903f4230409da8978d00037d99f2cb1335dadae7449e78a5daae5fe802bde9c1a24847
Homepage: https://github.com/brandon-rhodes/python-sgp4
Description-en: Track earth satellite TLE orbits using up-to-date 2010 version of sgp4
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 of the predictions of the standard C++ implementation 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.
.
The C++ function names have been retained, since users may already be familiar
with this library in other languages
Description-md5: 5866e668dc11a398a9c752fd71653ec7