AR725

Looking at the Restart states from Rev 727 we have the following results for AR725.
AR725		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)		
MMS2	Mar 13 2017 08:58:28.568	54642.483	60110.774	60112.838	5468.290	5470.354	-2.06403	-0.038%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS2	Mar 13 2017 08:58:28.568	2118.631	2444.490	2444.616	325.858	325.984	-0.12591	-7.55	
 
MMS2 was 35.06 m/s (net delta-v) using 22.90 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, MMS2 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)	
MMS2_AR725	2017_69/19:21:26.565 to 2017_69/20:23:26.565	-33.6557	-9.5596	-2.2251	
		0.336557	0.095596	0.022251	
		-0.09304	-0.03262	-0.04124