Very long computation time for NumericalPropagator with EquinoctialOrbit

I am trying to use NumericalPropagator with EquinoctialOrbit, and I am finding that when I try to retrieve initial conditions using getPVCoordinates with the initial time and an inertial frame OR when I try to use the propagate method with the initial time and a final time one hour later, my code just hangs and never produces a result. Any thoughts on the cause of my issue?
Thank you!

Hi @erinf,

Could you please share your code? It should not behave like this.


It seems that this issue is resolved. I am sorry that I don’t understand what I did to fix the issue, but somehow it is magically fixed! Thank you for your response.