diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.cpp b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.cpp
index 51c5415f11..0b5b6dd656 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.cpp
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.cpp
@@ -705,6 +705,7 @@ ARCore::ARCore(VESSEL* v, AR_GCore* gcin)
 	VECdirection = 0;
 	VECbody = NULL;
 	VECangles = _V(0, 0, 0);
+	VECBodyVector = _V(0, 0, 0);
 
 	TPI_Mode = 0;
 	dt_TPI_sunrise = 16.0*60.0;
@@ -2435,56 +2436,72 @@ void ARCore::VecPointCalc(bool IsCSM)
 
 		if (v == NULL) return;
 
-		VECTOR3 vPos, pPos, relvec, UX, UY, UZ, loc;
-		MATRIX3 M, M_R;
-		double p_T, y_T;
-		OBJHANDLE gravref = GC->rtcc->AGCGravityRef(v);
-
-		p_T = 0;
-		y_T = 0;
+		EphemerisData sv;
+		MATRIX3 MAT, REFSMMAT;
+		VECTOR3 POINTVSM, vPos, pPos, dPos, U_LOS, UNITY, SCAXIS, UTSA, UTSB, UTSAP, UTSBP;
+		double UTPIT, UTYAW, OMICRON;
 
-		if (VECdirection == 1)
-		{
-			p_T = PI;
-			y_T = 0;
-		}
-		else if (VECdirection == 2)
-		{
-			p_T = 0;
-			y_T = PI05;
-		}
-		else if (VECdirection == 3)
+		if (IsCSM)
 		{
-			p_T = 0;
-			y_T = -PI05;
+			REFSMMAT = GC->rtcc->EZJGMTX1.data[0].REFSMMAT;
 		}
-		else if (VECdirection == 4)
+		else
 		{
-			p_T = -PI05;
-			y_T = 0;
+			REFSMMAT = GC->rtcc->EZJGMTX3.data[0].REFSMMAT;
 		}
-		else if (VECdirection == 5)
+
+		switch (VECdirection)
 		{
-			p_T = PI05;
-			y_T = 0;
+		case 0: //+X
+			UTYAW = 0;
+			UTPIT = 0;
+			break;
+		case 1: //-X
+			UTYAW = 0;
+			UTPIT = PI;
+			break;
+		case 2: //Optics
+			UTYAW = 0;
+			UTPIT = -(PI05 - 0.5676353234);
+			break;
+		case 3: //SIM Bay
+			UTYAW = PI05;
+			UTPIT = 52.25*RAD;
+			break;
+		default: //Selectable
+			UTYAW = VECBodyVector.x;
+			UTPIT = VECBodyVector.y;
+			break;
 		}
 
+		//State vector used in calculation
+		sv = GC->rtcc->StateVectorCalcEphem(v);
+		POINTVSM = unit(crossp(sv.V, sv.R));
+
+		//Pointing vector
 		v->GetGlobalPos(vPos);
 		oapiGetGlobalPos(VECbody, &pPos);
-		v->GetRelativePos(gravref, loc);
+		dPos = pPos - vPos;
+		dPos = mul(GC->rtcc->SystemParameters.MAT_J2000_BRCS, _V(dPos.x, dPos.z, dPos.y));
+		U_LOS = unit(dPos);
+
+		//Artemis calculations
+		OMICRON = VECBodyVector.z;
+		UNITY = _V(0, 1, 0);
+		SCAXIS = _V(cos(UTYAW)*cos(UTPIT), sin(UTYAW)*cos(UTPIT), -sin(UTPIT));
 
-		relvec = unit(pPos - vPos);
-		relvec = mul(GC->rtcc->SystemParameters.MAT_J2000_BRCS, _V(relvec.x, relvec.z, relvec.y));
-		loc = mul(GC->rtcc->SystemParameters.MAT_J2000_BRCS, _V(loc.x, loc.z, loc.y));
+		UTSAP = crossp(SCAXIS, UNITY);
+		if (length(UTSAP) == 0.0) return;
+		UTSAP = unit(UTSAP);
 
-		UX = relvec;
-		UY = unit(crossp(UX, -loc));
-		UZ = unit(crossp(UX, crossp(UX, -loc)));
+		POINTVSM = unit(crossp(U_LOS, POINTVSM));
 
-		M_R = _M(UX.x, UX.y, UX.z, UY.x, UY.y, UY.z, UZ.x, UZ.y, UZ.z);
-		M = _M(cos(y_T)*cos(p_T), sin(y_T), -cos(y_T)*sin(p_T), -sin(y_T)*cos(p_T), cos(y_T), sin(y_T)*sin(p_T), sin(p_T), 0.0, cos(p_T));
+		UTSA = POINTVSM * cos(OMICRON) + unit(crossp(U_LOS, POINTVSM))*sin(OMICRON);
+		UTSB = U_LOS;
+		UTSBP = SCAXIS;
 
-		VECangles = OrbMech::CALCGAR(GC->rtcc->EZJGMTX1.data[0].REFSMMAT, mul(OrbMech::tmat(M), M_R));
+		MAT = OrbMech::AXISGEN(UTSAP, UTSBP, UTSA, UTSB);
+		VECangles = OrbMech::CALCGAR(REFSMMAT, MAT);
 	}
 	else if (VECoption == 1)
 	{
diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.h b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.h
index 3f5d8c1b37..faa32582e8 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.h
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ARCore.h
@@ -318,7 +318,8 @@ class ARCore {
 
 	//VECPOINT PAGE
 	int VECoption;		//0 = Point SC at body, 1 = Open hatch thermal control
-	int VECdirection;	//0 = +X, 1 = -X, 2 = +Y,3 = -Y,4 = +Z, 5 = -Z
+	int VECdirection;	//0 = +X, 1 = -X, 2 = Optics, 3 = SIM Bay, 4 = Selectable
+	VECTOR3 VECBodyVector; //Yaw, pitch for option 7 and Omicron
 	OBJHANDLE VECbody;	//handle for the desired body
 	VECTOR3 VECangles;	//IMU angles
 
diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.cpp b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.cpp
index 3c23841051..b3556aa3bf 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.cpp
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.cpp
@@ -6395,7 +6395,7 @@ void ApolloRTCCMFD::TwoImpulseOffset()
 
 void ApolloRTCCMFD::cycleVECDirOpt()
 {
-	if (G->VECdirection < 5)
+	if (G->VECdirection < 4)
 	{
 		G->VECdirection++;
 	}
@@ -6405,6 +6405,19 @@ void ApolloRTCCMFD::cycleVECDirOpt()
 	}
 }
 
+void ApolloRTCCMFD::menuVECPOINTSelectAttitude()
+{
+	if (G->VECdirection == 4)
+	{
+		GenericDouble2Input(&G->VECBodyVector.x, &G->VECBodyVector.y, "Select body yaw and pitch:", RAD, RAD);
+	}
+}
+
+void ApolloRTCCMFD::menuVECPOINTOmicron()
+{
+	GenericDoubleInput(&G->VECBodyVector.z, "Select omicron (SEF = 180, BEF = 0):", RAD);
+}
+
 void ApolloRTCCMFD::cycleVECPOINTOpt()
 {
 	if (G->VECoption < 1)
@@ -6425,9 +6438,9 @@ void ApolloRTCCMFD::vecbodydialogue()
 
 bool VECbodyInput(void *id, char *str, void *data)
 {
-	if (oapiGetGbodyByName(str) != NULL)
+	if (oapiGetObjectByName(str) != NULL)
 	{
-		((ApolloRTCCMFD*)data)->set_vecbody(oapiGetGbodyByName(str));
+		((ApolloRTCCMFD*)data)->set_vecbody(oapiGetObjectByName(str));
 		return true;
 	}
 	return false;
diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.h b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.h
index 2a7faf6191..d0ad88e641 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.h
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD.h
@@ -354,6 +354,8 @@ class ApolloRTCCMFD: public MFD2 {
 	void cycleVECDirOpt();
 	void vecbodydialogue();
 	void set_vecbody(OBJHANDLE body);
+	void menuVECPOINTSelectAttitude();
+	void menuVECPOINTOmicron();
 	void menuVECPOINTCalc();
 	void menuSetLDPPVectorTime();
 	void menuLSRadius();
diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD_Display.cpp b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD_Display.cpp
index 055053e0c3..ae38840085 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD_Display.cpp
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApolloRTCCMFD_Display.cpp
@@ -1821,30 +1821,30 @@ bool ApolloRTCCMFD::Update(oapi::Sketchpad *skp)
 				skp->Text(1 * W / 16, 6 * H / 14, Buffer, strlen(Buffer));
 			}
 
-			if (G->VECdirection == 0)
+			switch (G->VECdirection)
 			{
+			case 0:
 				skp->Text(1 * W / 16, 8 * H / 14, "+X", 2);
-			}
-			else if (G->VECdirection == 1)
-			{
+				break;
+			case 1:
 				skp->Text(1 * W / 16, 8 * H / 14, "-X", 2);
+				break;
+			case 2:
+				skp->Text(1 * W / 16, 8 * H / 14, "Optics", 6);
+				break;
+			case 3:
+				skp->Text(1 * W / 16, 8 * H / 14, "SIM Bay", 7);
+				break;
+			default:
+				skp->Text(1 * W / 16, 8 * H / 14, "Selectable", 10);
+				sprintf(Buffer, "Y: %+07.2lf°", G->VECBodyVector.x*DEG);
+				skp->Text(1 * W / 16, 10 * H / 14, Buffer, strlen(Buffer));
+				sprintf(Buffer, "P: %+07.2lf°", G->VECBodyVector.y*DEG);
+				skp->Text(1 * W / 16, 11 * H / 14, Buffer, strlen(Buffer));
+				break;
 			}
-			else if (G->VECdirection == 2)
-			{
-				skp->Text(1 * W / 16, 8 * H / 14, "+Y", 2);
-			}
-			else if (G->VECdirection == 3)
-			{
-				skp->Text(1 * W / 16, 8 * H / 14, "-Y", 2);
-			}
-			else if (G->VECdirection == 4)
-			{
-				skp->Text(1 * W / 16, 8 * H / 14, "+Z", 2);
-			}
-			else if (G->VECdirection == 5)
-			{
-				skp->Text(1 * W / 16, 8 * H / 14, "-Z", 2);
-			}
+			sprintf(Buffer, "O: %+07.2lf°", G->VECBodyVector.z*DEG);
+			skp->Text(1 * W / 16, 12 * H / 14, Buffer, strlen(Buffer));
 		}
 
 		sprintf(Buffer, "%+07.2f R", G->VECangles.x*DEG);
diff --git a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApollomfdButtons.cpp b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApollomfdButtons.cpp
index 544a2d72be..ef1d40036c 100644
--- a/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApollomfdButtons.cpp
+++ b/Orbitersdk/samples/ProjectApollo/src_rtccmfd/ApollomfdButtons.cpp
@@ -517,11 +517,11 @@ ApolloRTCCMFDButtons::ApolloRTCCMFDButtons()
 	static const MFDBUTTONMENU mnu15[] =
 	{
 		{ "CSM or LM", 0, 'P' },
-		{ "Pointing body", 0, 'P' },
+		{ "Object to point at", 0, 'P' },
 		{ "Vessel axis", 0, 'D' },
-		{ "", 0, ' ' },
-		{ "", 0, ' ' },
-		{ "", 0, ' ' },
+		{ "Choose the direction", 0, 'D' },
+		{ "Choose pitch and yaw", 0, 'E' },
+		{ "Choose omicron angle", 0, 'F' },
 
 		{ "Select Vessel", 0, 'T' },
 		{ "Calculate attitude", 0, 'C' },
@@ -535,10 +535,10 @@ ApolloRTCCMFDButtons::ApolloRTCCMFDButtons()
 
 	RegisterFunction("VES", OAPI_KEY_P, &ApolloRTCCMFD::CycleCSMOrLMSelection);
 	RegisterFunction("OPT", OAPI_KEY_G, &ApolloRTCCMFD::cycleVECPOINTOpt);
-	RegisterFunction("BOD", OAPI_KEY_P, &ApolloRTCCMFD::vecbodydialogue);
+	RegisterFunction("OBJ", OAPI_KEY_P, &ApolloRTCCMFD::vecbodydialogue);
 	RegisterFunction("DIR", OAPI_KEY_D, &ApolloRTCCMFD::cycleVECDirOpt);
-	RegisterFunction("", OAPI_KEY_E, &ApolloRTCCMFD::menuVoid);
-	RegisterFunction("", OAPI_KEY_F, &ApolloRTCCMFD::menuVoid);
+	RegisterFunction("PY", OAPI_KEY_E, &ApolloRTCCMFD::menuVECPOINTSelectAttitude);
+	RegisterFunction("OMI", OAPI_KEY_F, &ApolloRTCCMFD::menuVECPOINTOmicron);
 
 	RegisterFunction("SEL", OAPI_KEY_T, &ApolloRTCCMFD::set_Vessel);
 	RegisterFunction("CLC", OAPI_KEY_C, &ApolloRTCCMFD::menuVECPOINTCalc);