diff --git a/mission/controller/AcsController.cpp b/mission/controller/AcsController.cpp
index 67596fc9..f5f246c2 100644
--- a/mission/controller/AcsController.cpp
+++ b/mission/controller/AcsController.cpp
@@ -420,7 +420,7 @@ void AcsController::performPointingCtrl() {
 
   switch (mode) {
     case acs::PTG_IDLE:
-      guidance.targetQuatPtgIdle(timeDelta, timeAbsolute, susDataProcessed.sunIjkModel.value,
+      guidance.targetQuatPtgIdle(timeAbsolute, timeDelta, susDataProcessed.sunIjkModel.value,
                                  gpsDataProcessed.gpsPosition.value, targetQuat, targetSatRotRate);
       guidance.comparePtg(quatBI, rotRateB, targetQuat, targetSatRotRate, errorQuat,
                           errorSatRotRate, errorAngle);
diff --git a/mission/controller/acs/Guidance.cpp b/mission/controller/acs/Guidance.cpp
index e4e9ccab..3641e41e 100644
--- a/mission/controller/acs/Guidance.cpp
+++ b/mission/controller/acs/Guidance.cpp
@@ -4,7 +4,7 @@ Guidance::Guidance(AcsParameters *acsParameters_) { acsParameters = acsParameter
 
 Guidance::~Guidance() {}
 
-void Guidance::targetQuatPtgIdle(const double timeDelta, timeval timeAbsolute,
+void Guidance::targetQuatPtgIdle(timeval timeAbsolute, const double timeDelta,
                                  const double sunDirI[3], const double posSatF[4],
                                  double targetQuat[4], double targetSatRotRate[3]) {
   // positive z-Axis of EIVE in direction of sun
diff --git a/mission/controller/acs/Guidance.h b/mission/controller/acs/Guidance.h
index 973c0bd3..9835b762 100644
--- a/mission/controller/acs/Guidance.h
+++ b/mission/controller/acs/Guidance.h
@@ -25,7 +25,7 @@ class Guidance {
   ReturnValue_t solarArrayDeploymentComplete();
   void resetValues();
 
-  void targetQuatPtgIdle(const double timeDelta, timeval timeAbsolute, const double sunDirI[3],
+  void targetQuatPtgIdle(timeval timeAbsolute, const double timeDelta, const double sunDirI[3],
                          const double posSatF[4], double targetQuat[4], double targetSatRotRate[3]);
   void targetQuatPtgTarget(timeval timeAbsolute, const double timeDelta, double posSatF[3],
                            double velSatE[3], double quatIX[4], double targetSatRotRate[3]);