def test_visible_above_horizon(self):
        """
        visible_above_horizon test
        """
        #equitorial orbit
        tle_line1 = "1 44235U 19029A   20178.66667824  .02170155  00000-0  40488-1 0  9998"
        tle_line2 = "2 44235  00.0000 163.9509 0005249 306.3756  83.0170 15.45172567 61683"
        #high inclination orbit
        tle2_line1 = "1 44235U 19029A   20178.66667824  .02170155  00000-0  40488-1 0  9998"
        tle2_line2 = "2 44235  70.0000 163.9509 0005249 306.3756  83.0170 15.45172567 61683"
        prop1 = orekit_utils.str_tle_propagator(tle_line1, tle_line2)
        prop2 = orekit_utils.str_tle_propagator(tle2_line1, tle2_line2)
        time = AbsoluteDate(2020, 6, 26, 1, 40, 00.000,
                            TimeScalesFactory.getUTC())

        #verified with graphing overviews
        self.assertFalse(orekit_utils.visible_above_horizon(
            prop1, prop2, time))
        self.assertTrue(
            orekit_utils.visible_above_horizon(prop1, prop2,
                                               time.shiftedBy(60. * 10.)))
        self.assertTrue(
            orekit_utils.visible_above_horizon(
                prop1, prop2, time.shiftedBy(60. * 10. + 45. * 60.)))
        time_period_visible = orekit_utils.visible_above_horizon(
            prop1, prop2, time, 60 * 30)[0]
        self.assertTrue(
            time.shiftedBy(60. * 10.).isBetween(time_period_visible[0],
                                                time_period_visible[1]))
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    def test_find_sat_distance(self):
        """
        find_distance tests: test some well known distances and zero cases
        """
        tle_line1 = "1 25544U 98067A   20174.66385417  .00000447  00000-0  16048-4 0  9992"
        tle_line2 = "2 25544  51.6446 321.3575 0002606  75.8243 105.9183 15.49453790232862"
        tle2_line1 = "1 44235U 19029A   20178.58335648  .01685877  00000-0  31131-1 0  9991"
        tle2_line2 = "2 44235  52.9995 164.3403 0009519 291.6111 354.0622 15.45232749 61668"

        prop1 = orekit_utils.str_tle_propagator(tle_line1, tle_line2)
        prop2 = orekit_utils.str_tle_propagator(tle2_line1, tle2_line2)

        time = orekit_utils.absolute_time_converter_utc_string('2020-12-02T00:00:00.000')

        self.assertEqual(orekit_utils.find_sat_distance(prop1,prop2,time),orekit_utils.find_sat_distance(prop1,prop2,time))
        self.assertEqual(orekit_utils.find_sat_distance(prop1,prop1,time),0.)
        self.assertEqual(orekit_utils.find_sat_distance(prop2,prop2,time),0.)
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 def test_str_tle_propagator(self):
     tle_line1 = "1 25544U 98067A   20174.66385417  .00000447  00000-0  16048-4 0  9992"
     tle_line2 = "2 25544  51.6446 321.3575 0002606  75.8243 105.9183 15.49453790232862"
     propagator_1 = orekit_utils.str_tle_propagator(tle_line1, tle_line2)
     TLE = orekit_utils.convert_tle_string_to_TLE(tle_line1, tle_line2)
     propagator_2 = TLEPropagator.selectExtrapolator(TLE)
     time = absolute_time_converter_utc_string('2020-12-02T00:00:00.000')
     self.assertTrue(propagator_1.propagate(time).getOrbit().toString() == propagator_2.propagate(time).getOrbit().toString())
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 def test_check_iot_in_range(self):
     """
     check_iot_in_range test
     """
     tle_line1 = "1 44235U 19029A   20178.66667824  .02170155  00000-0  40488-1 0  9998"
     tle_line2 = "2 44235  00.0000 163.9509 0005249 306.3756  270.0170 15.45172567 61683"
     prop1 = orekit_utils.str_tle_propagator(tle_line1, tle_line2)
     lat = 0.
     lon = 0.
     alt = 10.
     time = AbsoluteDate(2020, 6, 26, 1, 40, 00.000, TimeScalesFactory.getUTC())
     self.assertTrue(check_iot_in_range(prop1, lat, lon, alt, time))
     self.assertFalse(check_iot_in_range(prop1, lat, lon, alt, time.shiftedBy(60.*30.)))