AR707

Looking at the Restart states from Rev 709 we have the following results for AR707.
AR707		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)			
MMS4	Feb 16 2017 15:23:00.374	44915.588	47449.044	47449.966	2533.456	2534.378	-0.92208	-0.04%	0.15%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS4	Feb 16 2017 15:23:00.374	1578.903	1714.356	1714.406	135.453	135.503	-0.04997	-2.998		
 
MMS4 was 25.55 m/s using 16.10 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, all 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_AR707	2017_45/20:12:16.22 to 2017_45/20:51:56.22	-24.659	-6.5564	-1.5649	
		0.24659	0.065564	0.015649	
		-0.042	-0.015	-0.024