AR722

Looking at the Restart states from Rev 724 we have the following results for AR722.
AR722		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)		
MMS3	Mar 08 2017 22:52:17.812	54648.513	60122.012	60123.165	5473.499	5474.652	-1.15263	-0.02%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS3	Mar 08 2017 22:52:17.812	2118.982	2445.175	2445.246	326.193	326.264	-0.07032	-4.22	
 
MMS3 was 34.93 m/s (net delta-v) using 22.80 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, MMS3 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)	
MMS3_AR722	2017_65/09:13:48.22 to 2017_65/10:15:38.22	-33.5823	-9.3853	-2.1257	
		0.335823	0.093853	0.021257	
		-0.01698	-0.01789	-0.007768