TwoBodyPropagator Constructor (JulianDate, ReferenceFrame, KeplerianElements)

public TwoBodyPropagator(
	JulianDate orbitEpoch,
	ReferenceFrame referenceFrame,
	KeplerianElements elements
)

Public Sub New ( 
	orbitEpoch As JulianDate,
	referenceFrame As ReferenceFrame,
	elements As KeplerianElements
)

public:
TwoBodyPropagator(
	JulianDate orbitEpoch, 
	ReferenceFrame^ referenceFrame, 
	KeplerianElements^ elements
)

new : 
        orbitEpoch : JulianDate * 
        referenceFrame : ReferenceFrame * 
        elements : KeplerianElements -> TwoBodyPropagator