AR720

Looking at the Restart states from Rev 722 we have the following results for AR720.
AR720		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)		
MMS4	Mar 05 2017 15:53:02.299	51105.275	54648.216	54649.390	3542.941	3544.115	-1.17355	-0.03%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS4	Mar 05 2017 15:53:02.299	1916.277	2118.965	2119.033	202.688	202.756	-0.06826	-4.10	
 
MMS4 was 27.22 m/s (net delta-v) using 16.75 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, MMS4 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)	
MMS4_AR720	2017_60/23:44:25.835 to 2017_61/00:31:39.835	-26.117	-7.4499	-1.8672	
		0.26117	0.074499	0.018672	
		-0.08799	-0.06047	-0.05635