# Path: skyfield/api.py
# N = E = +1.0
# S = W = -1.0


from skyfield import api
from __future__ import print_function, division

def test_sat_almanac_LEO():
    # Testcase from
    # https://github.com/skyfielders/astronomy-notebooks/blob/master/Solvers/Earth-Satellite-Passes.ipynb
    # with elevated horizon

    tle = ["TIANGONG 1",
           "1 37820U 11053A   14314.79851609  .00064249  00000-0  44961-3 0  5637",
           "2 37820  42.7687 147.7173 0010686 283.6368 148.1694 15.73279710179072"]

# Path: skyfield/api.py
# N = E = +1.0
# S = W = -1.0


# Path: skyfield/tests/test_satellite_events.py
from skyfield import api

from __future__ import print_function, division

def test_sat_almanac_LEO():
    # Testcase from
    # https://github.com/skyfielders/astronomy-notebooks/blob/master/Solvers/Earth-Satellite-Passes.ipynb
    # with elevated horizon

    tle = ["TIANGONG 1",
           "1 37820U 11053A   14314.79851609  .00064249  00000-0  44961-3 0  5637",
           "2 37820  42.7687 147.7173 0010686 283.6368 148.1694 15.73279710179072"]

    sat = api.EarthSatellite(*tle[1:3], name=tle[0])