diff --git a/spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv b/spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
index b1855e80..10175581 100644
--- a/spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
+++ b/spacecraft/FoxTelem_1.13e/CubeSatSim_rttelemetry.csv
@@ -1,11 +1,11 @@
 46,TYPE,FIELD,BITS,UNIT,CONVERSION,MODULE,MODULE_NUM,MODULE_LINE,LINE_TYPE,SHOMIN_NAME,DESCRIPTION
-0,MIN,BATT_A_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A,Battery A voltage (0-2.5V scale)
-1,MIN,BATT_B_V,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Cell A+B,Battery A+B voltage (0-3.3V scale)
-2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Cell A+B+C Voltage,Battery A+B+C voltage (0-5.0V scale)
+0,MIN,SENSOR2,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor2,STEM Payload Extra Sensor2
+1,MIN,SENSOR3,12,V,cubesatsim_voltage|FLOAT2,NONE,0,0,3,Sensor3,STEM Payload Extra Sensor3
+2,MIN,BATT_V,12,V,cubesatsim_voltage|FLOAT2,NONE,4,1,3,Battery Voltage,Battery Voltage
 3,MIN,SatelliteXAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,7,4,3,Acceleration,Acceleration around X Axis
 4,MIN,SatelliteYAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,8,4,3,Acceleration,Acceleration around Y Axis
 5,MIN,SatelliteZAxisAcceleration,12,g,cubesatsim_acceleration|FLOAT2,NONE,9,4,3,Acceleration,Acceleration around Z Axis
-6,MIN,TOTAL_BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Current,Total Battery DC current
+6,MIN,BATT_I,12,mA,cubesatsim_current,NONE,4,2,3,Battery Current,Battery current
 7,MIN,Temperature,12,C,cubesatsim_temperature,NONE,6,2,3,Temperature,STEM Payload Sensor Temperature
 8,MIN,PANEL_PLUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,7,1,3,Voltage,+X Panel
 9,MIN,PANEL_MINUS_X_V,12,V,cubesatsim_voltage|FLOAT2,NONE,10,1,3,Voltage,-X Panel
@@ -19,7 +19,7 @@
 17,MIN,PANEL_MINUS_Y_I,12,mA,cubesatsim_current,NONE,11,2,3,Current,-Y Panel
 18,MIN,PANEL_PLUS_Z_I,12,mA,cubesatsim_current,NONE,9,2,3,Current,+Z Panel
 19,MIN,PANEL_MINUS_Z_I,12,mA,cubesatsim_current,NONE,12,2,3,Current,-Z Panel
-20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery2 Voltage,Power Supply Voltage
+20,MIN,BATT2_V,12,V,cubesatsim_voltage|FLOAT2,NONE,5,1,3,Battery2 Voltage,Battery2 Voltage
 21,MIN,SPIN,12,rpm,cubesatsim_rpm,NONE,3,1,3,Spacecraft Spin,Calculated spin rate using solar cells
 22,MIN,Pressure,12,bar,cubesatsim_pressure,NONE,6,3,3,Pressure,STEM Payload Sensor Pressure
 23,MIN,Altitude,12,m,cubesatsim_altitude,NONE,6,4,3,Altitude,STEM Payload Sensor Altitude
@@ -31,8 +31,8 @@
 29,MIN,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation|INT,NONE,9,3,3,Rotation,Angular Veolcity around Z Axis
 30,MIN,Humidity,12,%,cubesatsim_temperature,NONE,6,5,3,Humidity,STEM Payload Sensor Humidity
 31,MIN,BATT2_I,12,mA,cubesatsim_current,NONE,5,2,3,Battery2 Current,Power Supply DC Current
-32,MIN,Sensor1,12,signed raw,cubesatsim_rpm,NONE,6,6,3,Sensor 1,STEM Payload Extra Sensor 1
-33,MIN,Sensor2,12,signed scaled,cubesatsim_rpm,NONE,6,7,3,Sensor 2,STEM Payload Extra Sensor 2
+32,MIN,DIODE_T,12,signed raw,cubesatsim_rpm,NONE,6,6,3,Diode Temperature,Diode Temperature
+33,MIN,Sensor1,12,signed scaled,cubesatsim_rpm,NONE,6,7,3,Sensor 1,STEM Payload Extra Sensor 1
 34,MIN,STEMPayloadStatus,1,-,17,NONE,6,1,0,STEM Payload Status,STEM Payload Board Status
 35,MIN,Nominal Mode,1,-,17,NONE,3,2,0,Nominal Mode, Nominal Mode (Not Safe Mode)
 36,MIN,PayloadStatus1,1,-,17,NONE,6,7,0,Exp 2,STEM Payload status 1 failure indicator