pylupnt.cart2coe

pylupnt.cart2coe(posvel: Annotated[numpy.typing.ArrayLike, numpy.float64, '[6, 1]'], GM: SupportsFloat | SupportsIndex) → Annotated[numpy.typing.NDArray[numpy.float64], '[6, 1]']

Convert a Cartesian state to classical orbital elements given GM [km^3/s^2].