AR739

Looking at the Restart states from Rev 740 we have the following results for AR739.
AR739		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	Apr 13 2017 22:12:26.102	74721.482	83561.076	83564.533	8839.594	8843.052	-3.45771	-0.039%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS2	Apr 13 2017 22:12:26.102	3387.879	4006.506	4006.754	618.626	618.875	-0.24868	-14.92	
 
MMS2 was 30.36 m/s (net delta-v) using 18.11 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 does not meet 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_AR739	2017_99/17:38:49.613 to 2017_99/18:31:39.613	-29.0079	-8.7024	-2.0199	
		0.290079	0.087024	0.020199	
		-0.4344	-0.206	-0.22231