AR709

Looking at the Restart states from Rev 711 we have the following results for AR709.
AR709		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 19 2017 00:52:09.479	44917.576	47450.837	47451.614	2533.261	2534.038	-0.77704	-0.03%	0.08%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS2	Feb 19 2017 00:52:09.479	1579.008	1714.453	1714.495	135.445	135.487	-0.04211	-2.527		
 
MMS2 was 25.49 m/s using 16.26 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_AR709	2017_48/05:38:13.501 to 2017_48/06:18:53.501	-24.6502	-6.6067	-1.698	
		0.2465	0.066067	0.01698	
		0.045	-0.015	0.01