Monte Orbital Propagation

Basic orbital propagation.
(C) 2019 Nabla Zero Labs
License: CC BY-NC 3.0 US

# Python Standard Library
from __future__ import print_function

# Monte Library
import Monte
from mpy.units import *  # safe to perform global import

# Populate the BOA with a standard dataset.
boa =["time", "frame", "body", "ephem/planet/de431"])

# Define initial and final times for the orbital propagation
tbeg = Monte.Epoch("01-Jan-2019 00:00:00.0000 ET")
tend = tbeg + 10 * day

Nabla Zero Labs publishes this material under the Creative Commons Attribution-NonCommercial 3.0 United States License (CC BY-NC 3.0 US).