This attribute retrieves the orbit epoch date and time, which is used to define an Initial State or Launch Segment of a Mission Control Sequence.
Astrogator_RM <Satellite Object Path> GetValue <Astrogator Object Path>.Epoch
Specify the Epoch date and time. Select from the standard options for a time unit of measure.
Initial State Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.InitialState.Epoch
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Initial_State.FinalState.Epoch
Launch Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Launch.Launch.Epoch
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Launch.InitialState.Epoch
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Launch.FinalState.Epoch
Propagate Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Propagate.InitialState.Epoch
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Propagate.FinalState.Epoch
Hold Segment
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.InitialState.Epoch
Astrogator_RM */Satellite/Satellite1 GetValue MainSequence.SegmentList.Hold.FinalState.Epoch
STK Programming Interface 11.0.1