AR734

Looking at the Restart states from Rev 736 we have the following results for AR734.
AR734		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)		
MMS1	Mar 31 2017 05:43:06.681	65374.469	74738.886	74743.332	9364.417	9368.863	-4.44570	-0.047%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS1	Mar 31 2017 05:43:06.681	2772.503	3389.063	3389.366	616.560	616.863	-0.30239	-18.14	
 
MMS1 was 40.16 m/s (net delta-v) using 26.21 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, MMS1 meets 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)	
MMS1_AR734	2017_86/16:24:45.814 to 2017_86/17:38:55.814	-38.5154	-11.1669	-2.4285	
		0.385154	0.111669	0.024285	
		-0.04906	-0.02213	-0.01887