AR719

Looking at the Restart states from Rev 721 we have the following results for AR719.
AR719		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)		
MMS1	Mar 04 2017 05:05:57.030	51104.037	54645.812	54647.512	3541.775	3543.476	-1.70075	-0.05%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS1	Mar 04 2017 05:05:57.030	1916.208	2118.825	2118.924	202.617	202.716	-0.09892	-5.94	
 
MMS1 was 27.16 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, MMS1 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)	
MMS1_AR719	2017_60/23:44:25.835 to 2017_61/00:31:39.835	-26. 07937	-7.37015	-1. 773582	
		0.2607937	0.0737015	0.01773582	
		-0.061	-0.04324	-0.0301