AR723

Looking at the Restart states from Rev 725 we have the following results for AR723.
AR723		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 10 2017 09:59:56.310	54647.753	60119.098	60121.205	5471.345	5473.452	-2.10657	-0.04%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS4	Mar 10 2017 09:59:56.310	2118.938	2444.997	2445.126	326.060	326.188	-0.12851	-7.71	
 
MMS4 was 35.06 m/s (net delta-v) using 22.70 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_AR723	2017_66/20:22:15.306 to 2017_66/21:22:45.306	-33.6996	-9.4563	-2.0368	
		0.336996	0.094563	0.020368	
		0.03642	-0.01379	0.02029