AR710

Looking at the Restart states from Rev 712 we have the following results for AR710.
AR710		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 20 2017 05:37:39.920	44918.615	47454.274	47455.203	2535.659	2536.588	-0.92914	-0.04%	0.15%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS1	Feb 20 2017 05:37:39.920	1579.062	1714.639	1714.689	135.577	135.627	-0.05036	-3.0215		
 
MMS1 was 25.45 m/s using 16.13 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_AR710	2017_49/10:25:39.884 to 2017_49/11:05:39.884	-24.5134	-6.66	-1.7855	
		0.245134	0.0666	0.017855	
		0.03	0.007	0.015