pylupnt.propagate_coe

pylupnt.propagate_coe(coe: Annotated[numpy.typing.ArrayLike, numpy.float64, '[6, 1]'], GM: SupportsFloat | SupportsIndex, dt: SupportsFloat | SupportsIndex) → Annotated[numpy.typing.NDArray[numpy.float64], '[6, 1]']

Propagate classical orbital elements by dt [s] under two-body motion.