AR730

Looking at the Restart states from Rev 731 we have the following results for AR730.
AR730		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 22 2017 21:05:15.565	60128.300	65391.445	65392.073	5263.144	5263.772	-0.62808	-0.012%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS3	Mar 22 2017 21:05:15.565	2445.559	2773.583	2773.623	328.024	328.064	-0.03996	-2.40	
 
MMS3 was 28.6 m/s (net delta-v) using 17.49 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_AR730	2017_78/23:20:05.492 to 2017_79/00:08:45.492	-27.371	-8.0074	-1.8854	
		0.27371	0.080074	0.018854	
		-0.02426	-0.01965	-0.00985