diff --git a/libraries/AP_NavEKF3/AP_NavEKF3.h b/libraries/AP_NavEKF3/AP_NavEKF3.h
index d7fefdccd3..025d5e8d22 100644
--- a/libraries/AP_NavEKF3/AP_NavEKF3.h
+++ b/libraries/AP_NavEKF3/AP_NavEKF3.h
@@ -524,6 +524,10 @@ private:
 
     bool inhibitGpsVertVelUse;  // true when GPS vertical velocity use is prohibited
 
+    // origin set by one of the cores
+    struct Location common_EKF_origin;
+    bool common_origin_valid;
+    
     // update the yaw reset data to capture changes due to a lane switch
     // new_primary - index of the ekf instance that we are about to switch to as the primary
     // old_primary - index of the ekf instance that we are currently using as the primary
diff --git a/libraries/AP_NavEKF3/AP_NavEKF3_Control.cpp b/libraries/AP_NavEKF3/AP_NavEKF3_Control.cpp
index b3ed8464eb..461148780a 100644
--- a/libraries/AP_NavEKF3/AP_NavEKF3_Control.cpp
+++ b/libraries/AP_NavEKF3/AP_NavEKF3_Control.cpp
@@ -479,10 +479,10 @@ bool NavEKF3_core::setOriginLLH(const Location &loc)
 }
 
 // Set the NED origin to be used until the next filter reset
-void NavEKF3_core::setOrigin()
+void NavEKF3_core::setOrigin(const Location &loc)
 {
     // assume origin at current GPS location (no averaging)
-    EKF_origin = AP::gps().location();
+    EKF_origin = loc;
     // if flying, correct for height change from takeoff so that the origin is at field elevation
     if (inFlight) {
         EKF_origin.alt += (int32_t)(100.0f * stateStruct.position.z);
@@ -491,7 +491,11 @@ void NavEKF3_core::setOrigin()
     // define Earth rotation vector in the NED navigation frame at the origin
     calcEarthRateNED(earthRateNED, EKF_origin.lat);
     validOrigin = true;
-    gcs().send_text(MAV_SEVERITY_INFO, "EKF3 IMU%u Origin set to GPS",(unsigned)imu_index);
+    gcs().send_text(MAV_SEVERITY_INFO, "EKF3 IMU%u origin set",(unsigned)imu_index);
+
+    // put origin in frontend as well to ensure it stays in sync between lanes
+    frontend->common_EKF_origin = EKF_origin;
+    frontend->common_origin_valid = true;
 }
 
 // record a yaw reset event
diff --git a/libraries/AP_NavEKF3/AP_NavEKF3_Measurements.cpp b/libraries/AP_NavEKF3/AP_NavEKF3_Measurements.cpp
index 5cc3db3878..aa388e0c8d 100644
--- a/libraries/AP_NavEKF3/AP_NavEKF3_Measurements.cpp
+++ b/libraries/AP_NavEKF3/AP_NavEKF3_Measurements.cpp
@@ -582,12 +582,17 @@ void NavEKF3_core::readGpsData()
             // Post-alignment checks
             calcGpsGoodForFlight();
 
+            // see if we can get an origin from the frontend
+            if (!validOrigin && frontend->common_origin_valid) {
+                setOrigin(frontend->common_EKF_origin);
+            }
+
             // Read the GPS location in WGS-84 lat,long,height coordinates
             const struct Location &gpsloc = gps.location();
 
             // Set the EKF origin and magnetic field declination if not previously set and GPS checks have passed
             if (gpsGoodToAlign && !validOrigin) {
-                setOrigin();
+                setOrigin(gpsloc);
 
                 // set the NE earth magnetic field states using the published declination
                 // and set the corresponding variances and covariances
diff --git a/libraries/AP_NavEKF3/AP_NavEKF3_core.h b/libraries/AP_NavEKF3/AP_NavEKF3_core.h
index 06aeb8d639..66f9217e91 100644
--- a/libraries/AP_NavEKF3/AP_NavEKF3_core.h
+++ b/libraries/AP_NavEKF3/AP_NavEKF3_core.h
@@ -768,7 +768,7 @@ private:
     void controlMagYawReset();
 
     // Set the NED origin to be used until the next filter reset
-    void setOrigin();
+    void setOrigin(const Location &loc);
 
     // determine if a takeoff is expected so that we can compensate for expected barometer errors due to ground effect
     bool getTakeoffExpected();