diff --git a/mission/controller/acs/Guidance.cpp b/mission/controller/acs/Guidance.cpp
index af9909c1..56355b42 100644
--- a/mission/controller/acs/Guidance.cpp
+++ b/mission/controller/acs/Guidance.cpp
@@ -409,10 +409,6 @@ void Guidance::sunQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *me
   double zAxis[3] = {0, 0, 0};
   VectorOperations<double>::normalize(sunDirB, zAxis, 3);
 
-  // Position of satellite in ECEF
-  double posSatE[3] = {0, 0, 0};
-  std::memcpy(gpsDataProcessed->gpsPosition.value, posSatE, 3 * sizeof(double));
-
   // Assign helper vector (north pole inertial)
   double helperVec[3] = {0, 0, 1};