TwoBodyPropagator Constructor (JulianDate, ReferenceFrame, EquinoctialElements) | 
 
            Initializes a new instance.
            
 
    Namespace: 
   AGI.Foundation.Propagators
    Assembly:
   AGI.Foundation.Models (in AGI.Foundation.Models.dll) Version: 25.1.421.0 (25.1.421.0)
Syntaxpublic TwoBodyPropagator(
	JulianDate orbitEpoch,
	ReferenceFrame referenceFrame,
	EquinoctialElements elements
)
Public Sub New ( 
	orbitEpoch As JulianDate,
	referenceFrame As ReferenceFrame,
	elements As EquinoctialElements
)
public:
TwoBodyPropagator(
	JulianDate orbitEpoch, 
	ReferenceFrame^ referenceFrame, 
	EquinoctialElements^ elements
)
new : 
        orbitEpoch : JulianDate * 
        referenceFrame : ReferenceFrame * 
        elements : EquinoctialElements -> TwoBodyPropagatorParameters
- orbitEpoch
 - Type: AGI.Foundation.TimeJulianDate
The Julian date at which the initial conditions are defined. - referenceFrame
 - Type: AGI.Foundation.GeometryReferenceFrame
            The reference frame in which the elements are defined.
            Generally this should be the InertialFrame of the central body
            around which you are propagating.  See the Remarks section for more information.
             - elements
 - Type: AGI.Foundation.CoordinatesEquinoctialElements
The elements from which to propagate. 
Remarks
See Also