diff --git a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
index b2369adb..1602cf7d 100755
--- a/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
+++ b/spacecraft/FoxTelem_1.09m/CubeSatSim_rttelemetryFM.csv
@@ -6,7 +6,7 @@
 4,RT,SatelliteYAxisAcceleration,12,g,cubesatsim_rotation,+Y Panel,7,4,3,Acceleration,Acceleration around Y Axis
 5,RT,SatelliteZAxisAcceleration,12,g,cubesatsim_rotation,+Z Panel,8,4,3,Acceleration,Acceleration around Z Axis
 6,RT,TOTAL_BATT_I,12,mA,cubesatsim_ina219_current,Battery,3,2,3,Current,Total Battery DC current
-7,RT,Temperature,12,C,8,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature
+7,RT,Temperature,12,C,cubesatsim_temperature,Experiments,5,2,3,Temp,STEM Payload Sensor Temperature
 8,RT,PANEL_PLUS_X_V,12,V,cubesatsim_ina219_voltage,+X Panel,6,2,3,Voltage,+X Panel
 9,RT,PANEL_MINUS_X_V,12,V,cubesatsim_ina219_voltage,-X Panel,9,2,3,Voltage,-X Panel
 10,RT,PANEL_PLUS_Y_V,12,V,cubesatsim_ina219_voltage,+Y Panel,7,2,3,Voltage,+YPanel
@@ -21,17 +21,17 @@
 19,RT,PANEL_MINUS_Z_I,12,mA,cubesatsim_ina219_current,-Z Panel,11,1,3,Current,-Z Panel
 20,RT,PSUVoltage,12,V,cubesatsim_ina219_voltage,PSU,4,2,3,Board Voltage,Power Supply Voltage
 21,RT,SPIN,12,rpm,12,Computer,2,2,3,Spacecraft Spin,Calculated spin rate using solar cells
-22,RT,Pressure,12,bar,10,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure
-23,RT,Altitude,12,m,7,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude
+22,RT,Pressure,12,bar,cubesatsim_pressure,Experiments,5,3,3,Pressure,STEM Payload Sensor Pressure
+23,RT,Altitude,12,m,cubesatsim_altitude,Experiments,5,4,3,Altitude,STEM Payload Sensor Altitude
 24,RT,RXTemperature,12,C,7,Radio,1,1,3,RX Temperature,Receiver card temperature
 25,RT,RSSI,12,dBm,14,Radio,1,2,3,RSSI,Received Signal Strength Indication
 26,RT,IHUTemperature,12,C,cubesatsim_temperature,Computer,2,1,3,Temperature,Internal Temperature of IHU
 27,RT,SatelliteXAxisAngularVelocity,12,dps,cubesatsim_rotation,+X Panel,6,3,3,Rotation,Angular Veolcity around X Axis
 28,RT,SatelliteYAxisAngularVelocity,12,dps,cubesatsim_rotation,+Y Panel,7,3,3,Rotation,Angular Veolcity around Y Axis
 29,RT,SatelliteZAxisAngularVelocity,12,dps,cubesatsim_rotation,+Z Panel,8,3,3,Rotation,Angular Veolcity around Z Axis
-30,RT,Sensor1,12,raw,7,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1
+30,RT,Sensor1,12,raw,cubesatsim_sensor1,Experiments,5,5,3,Sensor 1,STEM Payload Extra Sensor 1
 31,RT,PSUCurrent,12,mA,cubesatsim_ina219_current,PSU,4,1,3,Current,Power Supply DC Current
-32,RT,Sensor2,12,raw,7,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2
+32,RT,Sensor2,12,signed raw,cubesatsim_sensor2,Experiments,5,6,3,Sensor 2,STEM Payload Extra Sensor 2
 33,RT,Unused,20,na,7,NONE,0,0,0,Unused,Unused
 34,RT,Experiment1FailureIndication,1,-,17,Experiments,5,1,0,STEM Payload Status,STEM Payload Board Status
 35,RT,Experiment2FailureIndication,1,-,17,NONE,5,0,0,Not installed,Not used