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Fixup
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+97
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+97
-3
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astro_pi_orbit/__init__.py

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from .telemetry import ISS, de421, de440s, ephemeris
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__version__ = "2.0.0"
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__all__ = [
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"ISS",
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"de421",
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"de440s",
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"ephemeris",
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]

astro_pi_orbit/telemetry.py

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import os
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from pathlib import Path
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from skyfield.api import Loader, load
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_tle_dir: Path = Path(os.environ.get("TLE_DIR", Path.home()))
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print("_TLE_DIR", _tle_dir)
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_tle_filename = "iss.tle"
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_tle_url = "http://celestrak.com/NORAD/elements/stations.txt"
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_bsp_dir = os.environ.get("BSP_DIR", Path.home())
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print("_BSP_DIR", _bsp_dir)
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_bsp_421_filename = "de421.bsp"
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_bsp_440s_filename = "de440s.bsp"
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_timescale = load.timescale()
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def _load_iss():
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"""
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Retrieves ISS telemetry data from a local or remote TLE file and
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returns a Skyfield EarthSatellite object corresponding to the ISS.
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"""
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loader = Loader(_tle_dir, verbose=False)
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try:
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# find telemetry data locally
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satellites = loader.tle_file(_tle_filename)
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except FileNotFoundError:
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pass
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else:
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iss = next((sat for sat in satellites if sat.name == "ISS (ZARYA)"), None)
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if iss is None:
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raise RuntimeError(
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f"Unable to retrieve ISS TLE data from {loader.path_to(_tle_filename)}"
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)
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return iss
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try:
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# find telemetry data remotely
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satellites = loader.tle_file(_tle_url)
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Path(_tle_dir / Path(_tle_url).name).rename(_tle_dir / _tle_filename)
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except Exception as e:
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print(e)
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pass
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else:
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iss = next((sat for sat in satellites if sat.name == "ISS (ZARYA)"), None)
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if iss is None:
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raise RuntimeError(f"Unable to retrieve ISS TLE data from {_tle_url}")
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return iss
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raise FileNotFoundError(
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"Unable to retrieve ISS TLE data: "
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+ f"cannot find {loader.path_to(_tle_filename)} or download {_tle_url}."
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)
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def load_iss():
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ISS = _load_iss()
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# bind the `coordinates` function to the ISS object as a method
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setattr(ISS, "coordinates", coordinates.__get__(ISS, ISS.__class__))
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return ISS
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def coordinates(satellite):
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"""
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Return a Skyfield GeographicPosition object corresponding to the Earth
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latitude and longitude beneath the current celestial position of the ISS.
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See: rhodesmill.org/skyfield/api-topos.html#skyfield.toposlib.GeographicPosition
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"""
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return satellite.at(_timescale.now()).subpoint()
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def load_ephemeris(bsp_filename):
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loader = Loader(_bsp_dir, verbose=False)
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return loader(bsp_filename)
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# create ISS as a Skyfield EarthSatellite object
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# See: rhodesmill.org/skyfield/api-satellites.html#skyfield.sgp4lib.EarthSatellite
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ISS = load_iss
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# Expose ephemeris in the API
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de421 = load_ephemeris(_bsp_421_filename)
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de440s = load_ephemeris(_bsp_440s_filename)
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ephemeris = de421

scripts/ci.py

+1-1
Original file line numberDiff line numberDiff line change
@@ -98,5 +98,5 @@ def run_build(venv: ResolvedVenv):
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if __name__ == "__main__":
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venv: ResolvedVenv = prepare_venv(find_python())
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run_tests(venv)
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# run_tests(venv)
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run_build(venv)

test/test_astro_pi_orbit.py

-2
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