AR733

Looking at the Restart states from Rev 735 we have the following results for AR733.
AR733		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)		
MMS4	Mar 29 2017 06:56:04.928	65374.323	74715.789	74718.527	9341.466	9344.204	-2.73784	-0.029%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS4	Mar 29 2017 06:56:04.928	2772.494	3387.492	3387.678	614.999	615.185	-0.18620	-11.17	
 
MMS4 was 40.17 m/s (net delta-v) using 25.97 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, MMS4 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)	
MMS4_AR733	2017_84/17:40:07.515 to 2017_84/18:52:47.515	-38.5528	-11.1149	-2.3745	
		0.385528	0.111149	0.023745	
		-0.2329	-0.04417	-0.09531