Initializes a new instance. By default, Earth's inertial frame will be used as the propagation frame, the identity quaternion will be used as the initial attitude,
the zero vector will be used as the initial angular velocity, and the identity matrix will be used as the inertia matrix.
AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 23.2.417.0 (23.2.417.0)
new : unit -> PropagationEulerianAxes