AR724

Looking at the Restart states from Rev 726 we have the following results for AR724.
AR724		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 11 2017 21:50:43.292	54645.693	60114.042	60116.444	5468.349	5470.751	-2.40230	-0.044%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS1	Mar 11 2017 21:50:43.292	2118.818	2444.689	2444.836	325.871	326.018	-0.14654	-8.79	
 
MMS1 was 34.96 m/s (net delta-v) using 22.77 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_AR724	2017_68/08:13:26.939 to 2017_68/09:14:46.939	-33.5832	-9.4866	-2.1233	
		0.335832	0.094866	0.021233	
		0.03469	-0.01882	-0.02628