AR728

Looking at the Restart states from Rev 730 we have the following results for AR728.
AR728		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 19 2017 01:00:54.555	60118.969	65378.994	65381.518	5260.026	5262.549	-2.52357	-0.048%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS1	Mar 19 2017 01:00:54.555	2444.990	2772.791	2772.951	327.801	327.962	-0.16054	-9.63	
 
MMS1 was 28.7 m/s (net delta-v) using 17.52 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_AR728	2017_75/03:18:39.117 to 2017_75/04:06:59.117	-27.483	-8.0101	-1.7594	
		0.27483	0.080101	0.017594	
		-0.1848	-0.1088	-0.1038