TLE-tools is a small library to work with two-line element
set files.
The purpose of the library is to parse TLE sets into convenient TLE objects,
load entire TLE set files into pandas.DataFrame's, convert TLE objects into
poliastro.twobody.Orbit's, and more.
From Wikipedia:
A two-line element set (TLE) is a data format encoding a list of orbital elements of an Earth-orbiting object for a given point in time, the epoch. The TLE data representation is specific to the simplified perturbations models (SGP, SGP4, SDP4, SGP8 and SDP8), so any algorithm using a TLE as a data source must implement one of the SGP models to correctly compute the state at a time of interest. TLEs can describe the trajectories only of Earth-orbiting objects.
Example:
ISS (ZARYA)
1 25544U 98067A 19249.04864348 .00001909 00000-0 40858-4 0 9990
2 25544 51.6464 320.1755 0007999 10.9066 53.2893 15.50437522187805
Here is a minimal example on how to load the previous TLE:
from tletools import TLE tle_string = """ ISS (ZARYA) 1 25544U 98067A 19249.04864348 .00001909 00000-0 40858-4 0 9990 2 25544 51.6464 320.1755 0007999 10.9066 53.2893 15.50437522187805 """ tle_lines = tle_string.strip().splitlines() tle = TLE.from_lines(*tle_lines)
Then tle is:
TLE(name='ISS (ZARYA)', norad='25544', classification='U', int_desig='98067A', epoch_year=2019, epoch_day=249.04864348, dn_o2=1.909e-05, ddn_o6=0.0, bstar=4.0858e-05, set_num=999, inc=51.6464, raan=320.1755, ecc=0.0007999, argp=10.9066, M=53.2893, n=15.50437522, rev_num=18780)
and you can then access its attributes like t.argp, t.epoch...
Some more or less complete TLE format specifications can be found on the following websites:
Install and update using pip:
pip install -U TLE-tools
- Website: https://federicostra.github.io/tletools
- Documentation: https://tletools.readthedocs.io
- Releases: https://pypi.org/project/TLE-tools
- Code: https://github.com/FedericoStra/tletools
- Issue tracker: https://github.com/FedericoStra/tletools/issues