AR713

Looking at the Restart states from Rev 715 we have the following results for AR713.
AR713		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Feb 24 2017 00:25:02.213	47456.212	51106.992	51108.166	3650.780	3651.955	-1.17470	-0.03%	0.07%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS1	Feb 24 2017 00:25:02.213	1714.744	1916.374	1916.440	201.630	201.696	-0.06607	-3.96		
 
MMS1 was 31.68 m/s using 20.71 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_AR713	2017_53/00:01:44.804 to 2017_53/00:57:04.804	-30.5459	-8.3362	-2.0815	
		0.305459	0.083362	0.020815	
		-0.1556	-0.04851	-0.07666