This attribute retrieves the values for Target Vector Outgoing Asymptote elements used to define the spacecraft's Initial State.
Astrogator_RM <Satellite Object Path> GetValue <Astrogator Object Path>.Target_Vector_Outgoing_Asymptote.{Element}
If you select Target Vector Outgoing Asymptote as the Coordinate Type, the elements to be specified are the same as those for the Target Vector Incoming Asymptote type, except that Right Ascension and Declination are defined in terms of the outgoing rather than the incoming asymptote.
Initial State Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.InitialState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.InitialState.Target_Vector_Outgoing_Asymptote.rp
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.FinalState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.FinalState.Target_Vector_Outgoing_Asymptote.rp
Hold Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.InitialState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.InitialState.Target_Vector_Outgoing_Asymptote.rp
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.FinalState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.FinalState.Target_Vector_Outgoing_Asymptote.rp
Maneuver Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.InitialState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.InitialState.Target_Vector_Outgoing_Asymptote.rp
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.FinalState.Target_Vector_Outgoing_Asymptote
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Maneuver.FinalState.Target_Vector_Outgoing_Asymptote.rp
STK Programming Interface 11.0.1