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|
%global _empty_manifest_terminate_build 0
Name: python-TLE-tools
Version: 0.2.3
Release: 1
Summary: Library to work with two-line element set files
License: MIT
URL: https://federicostra.github.io/tletools
Source0: https://mirrors.aliyun.com/pypi/web/packages/8c/94/78c82e616e22eeb430089c73c5bd222b1a482943dec3aaf2ebb13f1eb001/TLE-tools-0.2.3.tar.gz
BuildArch: noarch
Requires: python3-attrs
Requires: python3-numpy
Requires: python3-pandas
Requires: python3-astropy
Requires: python3-poliastro
Requires: python3-pytest
Requires: python3-coverage
Requires: python3-tox
Requires: python3-sphinx
Requires: python3-pallets-sphinx-themes
Requires: python3-sphinxcontrib-log-cabinet
Requires: python3-sphinx-issues
Requires: python3-sphinx
Requires: python3-sphinx-rtd-theme
%description
# TLE-tools
`TLE-tools` is a small library to work with [two-line element
set](https://en.wikipedia.org/wiki/Two-line_element_set) files.
## Purpose
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](https://en.wikipedia.org/wiki/Two-line_element_set):
> 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](https://en.wikipedia.org/wiki/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:
```python
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:
```python
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`...
### TLE format specification
Some more or less complete TLE format specifications can be found on the following websites:
- [Wikipedia](https://en.wikipedia.org/wiki/Two-line_element_set#Format)
- [NASA](https://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html)
- [CelesTrak](https://celestrak.com/columns/v04n03/)
- [Space-Track](https://www.space-track.org/documentation#tle)
## Installation
Install and update using [pip](https://pip.pypa.io/en/stable/):
```bash
pip install -U TLE-tools
```
## Links
- 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
%package -n python3-TLE-tools
Summary: Library to work with two-line element set files
Provides: python-TLE-tools
BuildRequires: python3-devel
BuildRequires: python3-setuptools
BuildRequires: python3-pip
%description -n python3-TLE-tools
# TLE-tools
`TLE-tools` is a small library to work with [two-line element
set](https://en.wikipedia.org/wiki/Two-line_element_set) files.
## Purpose
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](https://en.wikipedia.org/wiki/Two-line_element_set):
> 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](https://en.wikipedia.org/wiki/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:
```python
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:
```python
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`...
### TLE format specification
Some more or less complete TLE format specifications can be found on the following websites:
- [Wikipedia](https://en.wikipedia.org/wiki/Two-line_element_set#Format)
- [NASA](https://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html)
- [CelesTrak](https://celestrak.com/columns/v04n03/)
- [Space-Track](https://www.space-track.org/documentation#tle)
## Installation
Install and update using [pip](https://pip.pypa.io/en/stable/):
```bash
pip install -U TLE-tools
```
## Links
- 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
%package help
Summary: Development documents and examples for TLE-tools
Provides: python3-TLE-tools-doc
%description help
# TLE-tools
`TLE-tools` is a small library to work with [two-line element
set](https://en.wikipedia.org/wiki/Two-line_element_set) files.
## Purpose
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](https://en.wikipedia.org/wiki/Two-line_element_set):
> 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](https://en.wikipedia.org/wiki/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:
```python
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:
```python
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`...
### TLE format specification
Some more or less complete TLE format specifications can be found on the following websites:
- [Wikipedia](https://en.wikipedia.org/wiki/Two-line_element_set#Format)
- [NASA](https://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html)
- [CelesTrak](https://celestrak.com/columns/v04n03/)
- [Space-Track](https://www.space-track.org/documentation#tle)
## Installation
Install and update using [pip](https://pip.pypa.io/en/stable/):
```bash
pip install -U TLE-tools
```
## Links
- 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
%prep
%autosetup -n TLE-tools-0.2.3
%build
%py3_build
%install
%py3_install
install -d -m755 %{buildroot}/%{_pkgdocdir}
if [ -d doc ]; then cp -arf doc %{buildroot}/%{_pkgdocdir}; fi
if [ -d docs ]; then cp -arf docs %{buildroot}/%{_pkgdocdir}; fi
if [ -d example ]; then cp -arf example %{buildroot}/%{_pkgdocdir}; fi
if [ -d examples ]; then cp -arf examples %{buildroot}/%{_pkgdocdir}; fi
pushd %{buildroot}
if [ -d usr/lib ]; then
find usr/lib -type f -printf "\"/%h/%f\"\n" >> filelist.lst
fi
if [ -d usr/lib64 ]; then
find usr/lib64 -type f -printf "\"/%h/%f\"\n" >> filelist.lst
fi
if [ -d usr/bin ]; then
find usr/bin -type f -printf "\"/%h/%f\"\n" >> filelist.lst
fi
if [ -d usr/sbin ]; then
find usr/sbin -type f -printf "\"/%h/%f\"\n" >> filelist.lst
fi
touch doclist.lst
if [ -d usr/share/man ]; then
find usr/share/man -type f -printf "\"/%h/%f.gz\"\n" >> doclist.lst
fi
popd
mv %{buildroot}/filelist.lst .
mv %{buildroot}/doclist.lst .
%files -n python3-TLE-tools -f filelist.lst
%dir %{python3_sitelib}/*
%files help -f doclist.lst
%{_docdir}/*
%changelog
* Fri Jun 09 2023 Python_Bot <Python_Bot@openeuler.org> - 0.2.3-1
- Package Spec generated
|
