Index: trunk/BNS/RTCM/clock_orbit_rtcm.c
===================================================================
--- trunk/BNS/RTCM/clock_orbit_rtcm.c	(revision 878)
+++ trunk/BNS/RTCM/clock_orbit_rtcm.c	(revision 1205)
@@ -3,5 +3,5 @@
         Name:           clock_orbit_rtcm.c
         Project:        RTCM3
-        Version:        $Id$
+        Version:        $Id: clock_orbit_rtcm.c,v 1.3 2008/08/15 16:29:40 weber Exp $
         Authors:        Dirk Stöcker
         Description:    state space approach for RTCM3
@@ -495,4 +495,6 @@
     if(!co) return GCOBR_NOCLOCKORBITPARAMETER;
     G_GPS_EPOCH_TIME(co->GPSEpochTime, co->NumberOfGPSSat)
+    co->epochGPS[co->epochSize] = co->GPSEpochTime;   /* Weber, for latency */
+    if(co->epochSize < 100) {co->epochSize += 1;}     /* Weber, for latency */
     G_MULTIPLE_MESSAGE_INDICATOR(mmi)
     G_RESERVED6
@@ -521,4 +523,6 @@
     if(!co) return GCOBR_NOCLOCKORBITPARAMETER;
     G_GPS_EPOCH_TIME(co->GPSEpochTime, co->NumberOfGPSSat)
+    co->epochGPS[co->epochSize] = co->GPSEpochTime;   /* Weber, for latency */
+    if(co->epochSize < 100) {co->epochSize += 1;}     /* Weber, for latency */
     G_MULTIPLE_MESSAGE_INDICATOR(mmi)
     G_RESERVED6
@@ -539,4 +543,6 @@
     if(!co) return -5;
     G_GPS_EPOCH_TIME(co->GPSEpochTime, co->NumberOfGPSSat)
+    co->epochGPS[co->epochSize] = co->GPSEpochTime;   /* Weber, for latency */
+    if(co->epochSize < 100) {co->epochSize += 1;}     /* Weber, for latency */
     G_MULTIPLE_MESSAGE_INDICATOR(mmi)
     G_RESERVED6
Index: trunk/BNS/RTCM/clock_orbit_rtcm.h
===================================================================
--- trunk/BNS/RTCM/clock_orbit_rtcm.h	(revision 878)
+++ trunk/BNS/RTCM/clock_orbit_rtcm.h	(revision 1205)
@@ -6,5 +6,5 @@
         Name:           clock_orbit_rtcm.h
         Project:        RTCM3
-        Version:        $Id$
+        Version:        $Id: clock_orbit_rtcm.h,v 1.3 2008/08/15 16:29:19 weber Exp $
         Authors:        Dirk Stöcker
         Description:    state space approach for RTCM3
@@ -52,4 +52,6 @@
   int ClockDataSupplied;            /* boolean */
   int OrbitDataSupplied;            /* boolean */
+  int epochGPS[101];                /* Weber, for latency */
+  int epochSize;                    /* Weber, for latency */
   enum SatelliteReferencePoint SatRefPoint;
   enum SatelliteReferenceDatum SatRefDatum;
