AR714

Looking at the Restart states from Rev 716 we have the following results for AR714.
AR714		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)			
MMS2	Feb 25 2017 04:48:34.692	47452.582	51103.783	51104.987	3651.200	3652.404	-1.20422	-0.03%	0.03%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS2	Feb 25 2017 04:48:34.692	1714.547	1916.193	1916.261	201.646	201.714	-0.06773	-4.06		
 
MMS2 was 31.74 m/s using 20.88 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_AR714	2017_54/04:27:33.885 to 2017_54/05:21:13.885	-30.5768	-8.2827	-1.9812	
		0.305768	0.082827	0.019812	
		-0.281	-0.06626	-0.1353