AR736

Looking at the Restart states from Rev 738 we have the following results for AR736.
AR736		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)		
MMS1	Apr 05 2017 14:12:03.061	74753.880	83584.663	83588.926	8830.783	8835.046	-4.26296	-0.048%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS1	Apr 05 2017 14:12:03.061	3390.083	4008.202	4008.509	618.119	618.426	-0.30664	-18.40	
 
MMS1 was 30.06 m/s (net delta-v) using 17.96 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_AR736	2017_91/09:32:33.212 to 2017_91/10:24:33.212	-28.7692	-8.5058	-1.8507	
		0.287692	0.085058	0.018507	
		-0.02678	-0.02828	-0.01303