AR708

Looking at the Restart states from Rev 710 we have the following results for AR708.
AR708		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS3	Feb 17 2017 20:07:00.029	44915.730	47449.942	47450.710	2534.213	2534.980	-0.76746	-0.03%	0.08%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS3	Feb 17 2017 20:07:00.029	1578.910	1714.404	1714.446	135.494	135.536	-0.04159	-2.496		
 
MMS3 was 25.49 m/s using 16.17 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, only the DVZ 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)	
MMS3_AR708	2017_47/00:55:43.12 to 2017_47/01:36:13.12	-24.5839	-6.5598	-1.6253	
		0.245839	0.065598	0.016253	
		-0.175	-0.05	-0.09