Several methods of Astrogator plugin components pass this component as the lone argument.  This component contains functions that allow the plugin component to access inputs.

Date	DEPRECATED. Use DateElements instead. Current epoch in requested time scale expressed in date format.
Date_Array	DEPRECATED. Use DateElements_Array instead. Current epoch in requested time scale expressed in date format returned as an array representing year [yyyy], dayOfYear, month [0-11], hour [0-23], minute [0-59], seconds. Useful for scripting clients.
DateElements	Current epoch in requested time scale expressed in date format. Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60].
DateElements_Array	Current epoch in requested time scale expressed in date format returned as the array: Year [yyyy], DayOfYear [1-366], Month [1-12], DayOfMonth [1-31], Hour [0-23], Minute [0-59], Seconds [0-60]. Useful for scripting clients.
DateString	Current epoch expressed using the date format abbreviation specified.
DayCount	Current epoch in requested time scale expressed in day count format.
DayCount_Array	Current epoch in requested time scale expressed in day count format returned as an array representing wholeDays, secsIntoDay. Useful for scripting clients.
IndicateEvent	Marks an event to the propagator.
LatLonAlt	Current detic latitude, detic longitude, and altitude.
LatLonAlt_Array	Current detic latitude, detic longitude, and altitude(in internal units) returned as an array representing lat, lon, alt. Useful for scripting clients.
PosVel	Current position and velocity in the requested frame.
PosVel_Array	Current position and velocity in the requested frame (in internal units) returned as an array representing x, y, z, vx, vy, vz. Useful for scripting clients.
SetColor	Sets the segment color.
SetMaxStep	Sets the maximum step size for the propagator.
StopPropagation	Stops propagation. For fatal errors.
SunPosition	Position of the sun wrt the current satellite position, in the requested frame, computed in the requested manner.
SunPosition_Array	Position of the sun wrt the current satellite position, in the requested frame, computed in the requested manner, (in internal units) returned as an array representing x, y, z. Useful for scripting clients.
Trace	Set this interface to trace the next numCalls by outputting a message to the message viewer.
TransformVector	Transforms a vector from the input frame to the output frame.
TransformVector_Array	Transforms a vector from the input frame to the output frame (in internal units) returned as an array representing x, y, z. Useful for scripting clients.

Altitude	Current altitude.
CbName	Name of the central body used as reference frame origin.
Cd	Drag Coefficient.
Cr	SRP Coefficient.
DragArea	Drag Area.
DryMass	Dry Mass.
FuelMass	Fuel Mass.
Mass	Total Mass.
Mu	Gravitational constant of the state central body
SRPArea	SRP Area.

Name
AgGatorPluginResultState