![]() ![]() ![]() Initial_date = AbsoluteDate(dt_utc_now.year,įinal_date = extrap_date.shiftedBy(3600. However, it does not affect the conclusion from this simulation.Ĭonfig = ['1 44057U 19010A 21242.77040566. Note that for Walker Star constellation, should use a seed satellite from "plane 1". Attached please find my codeįrom orekit.pyhelpers import setup_orekit_curdir, absolutedate_to_datetimeįrom .tle import TLE, TLEPropagatorįrom import KeplerianPropagatorįrom import ElevationDetector, EventsLoggerįrom .handlers import ContinueOnEventįrom import PropagatorsParallelizer, SpacecraftState, PythonAdditionalStateProviderįrom import PythonMultiSatStepHandlerįrom import CartesianOrbit, KeplerianOrbit, OrbitType, PositionAngleįrom import FramesFactory, TopocentricFrameįrom import Constants, IERSConventionsįrom import OneAxisEllipsoid, GeodeticPointįrom import TimeScalesFactory, AbsoluteDate I did import the same conda env from my laptop to my desktop. _ = parallelizer.propagate(extrap_date, final_date)Īt .PythonMultiSatStepHandler.handleStep(Native Method)Īt .propagate(PropagatorsParallelizer.java:180) However, when I am launching the same script from my new desktop, I am hitting the following JavaError: I have found the other script about PropagatorsParallelizer very helpful and was able to get my script running on my laptop. I am playing with a script about the visibility of 2 Walker constellations from 2 ground stations using PropagatorsParallelizer. ![]()
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