AR727

Looking at the Restart states from Rev 729 we have the following results for AR727.
AR727		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)		
MMS2	Mar 17 2017 02:38:42.516	60112.862	65369.862	65371.657	5257.000	5258.795	-1.79543	-0.034%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS2	Mar 17 2017 02:38:42.516	2444.617	2772.210	2772.324	327.593	327.707	-0.11421	-6.85	
 
MMS2 was 28.7 m/s (net delta-v) using 17.59 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, MMS2 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)	
MMS2_AR727	2017_73/04:57:00.539 to 2017_73/05:45:50.539	-27.5269	-7.9787	-1.6955	
		0.275269	0.079787	0.016955	
		0.5681	0.05664	0.2196