AR731

Looking at the Restart states from Rev 733 we have the following results for AR731.
AR731		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 25 2017 10:57:51.945	65378.980	74724.898	74728.588	9345.919	9349.608	-3.68932	-0.039%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS2	Mar 25 2017 10:57:51.945	2772.790	3388.112	3388.363	615.322	615.573	-0.25092	-15.05	
 
MMS2 was 39.78 m/s (net delta-v) using 26.13 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, 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_AR731	2017_80/21:35:50.89 to 2017_80/22:50:20.89	-38.187	-10.8899	-2.3177	
		0.38187	0.108899	0.023177	
		-0.01294	0.004768	-0.00412