AR718

Looking at the Restart states from Rev 720 we have the following results for AR718.
AR718		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)		
MMS2	Mar 02 2017 17:26:44.463	51101.177	54643.004	54643.893	3541.826	3542.716	-0.88977	-0.03%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS2	Mar 02 2017 17:26:44.463	1916.047	2118.662	2118.713	202.615	202.667	-0.05175	-3.10	
 
MMS2 was 27.19 m/s (net delta-v) using 16.98 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_AR718	2017_59/12:17:11.902 to 2017_59/13:02:01.902	-26.1305	-7.3307	-1.6963	
		0.261305	0.073307	0.016963	
		0.0328	-0.02061	0.01661