AR732

Looking at the Restart states from Rev 734 we have the following results for AR732.
AR732		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	Mar 27 2017 08:53:41.222	65367.178	74705.655	74707.699	9338.476	9340.521	-2.04465	-0.022%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS3	Mar 27 2017 08:53:41.222	2772.039	3386.803	3386.942	614.764	614.903	-0.13904	-8.34	
 
MMS3 was 39.85 m/s (net delta-v) using 26.17 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 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)	
MMS3_AR732	2017_82/19:36:07.993 to 2017_82/20:50:37.993	-38.2582	-10.9237	-2.2584	
		0.382582	0.109237	0.022584	
		-0.102	-0.02116	-0.04443