AR738

Looking at the Restart states from Rev 740 we have the following results for AR738.
AR738		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS3	Apr 11 2017 03:10:57.209	74713.027	83551.079	83552.759	8838.051	8839.731	-1.68018	-0.019%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS3	Apr 11 2017 03:10:57.209	3387.304	4005.787	4005.908	618.482	618.603	-0.12083	-7.25	
 
MMS3 was 30.26 m/s (net delta-v) using 18.07 kg
The Table below provides the following information:
•	First row for each maneuver: planned maneuver total delta-V values based on the associated DVTABLEs  
•	Second row for each maneuver: associated final maneuver p lanning requirements 
•	Third row for each maneuver: predicted velocity error at the time of the maneuver computed by differencing the predicted velocity at the maneuver time (starting with the post-perigee GEONS state prior to the maneuver) vs the definitive GEONS state at the time of the maneuver.
As shown in the table below, MMS3 does not meet the requirement 
Maneuver ID	Timespan	DVX (m/s)/ 
Req. (m/s)/
DiffVX(m/s)	DVY (m/s)/
Req. (m/s)/
DiffVY(m/s)	DVZ (m/s)/
Req. (m/s)/
DiffVZ(m/s)	
MMS3_AR738	2017_96/22:36:32.461 to 2017_96/23:29:12.461	-28.925	-8.6195	-1.9522	
		0.28925	0.086195	0.019522	
		-0.4797	-0.2755	-0.2751