AR737

Looking at the Restart states from Rev 739 we have the following results for AR737.
AR737		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)		
MMS4	Apr 08 2017 08:20:46.049	74731.780	83564.112	83566.621	8832.332	8834.840	-2.50862	-0.028%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS4	Apr 08 2017 08:20:46.049	3388.580	4006.724	4006.904	618.144	618.325	-0.18043	-10.83	
 
MMS4 was 30.17 m/s (net delta-v) using 17.87 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, MMS4 does not meet the requirement for DVY and DVZ
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)	
MMS4_AR737	2017_94/03:44:02.089 to 2017_94/04:35:02.089	-28.8528	-8.6	-1.9146	
		0. 288528	0.086	0.019146	
		-0.1694	-0.09538	-0.1003