AR717

Looking at the Restart states from Rev 718 we have the following results for AR717.
AR717		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 01 2017 06:08:08.890	51098.423	54640.273	54641.769	3541.850	3543.346	-1.49628	-0.04%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS3	Mar 01 2017 06:08:08.890	1915.892	2118.503	2118.590	202.611	202.698	-0.08702	-5.22	
 
MMS3 was 27.15 m/s (net delta-v) using 16.86 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_AR717	2017_58/00:48:47.588 to 2017_58/01:33:37.588	-26.1068	-7.2799	-1.6198	
		0.261068	0.072799	0.016198	
		-0.003661	-0.0123	-0.0008273