AR705

Looking at the Restart states from Rev 706 we have the following results for AR705.
AR705		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 14 2017 07:21:59.176	42108.754	44914.566	44915.595	2805.812	2806.841	-1.02870	-0.04%	0.14%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS4	Feb 14 2017 07:21:59.176	1433.238	1578.849	1578.903	145.611	145.665	-0.05424	-3.25		
 
MMS4 was 31.37 m/s using 20.79 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_AR705	2017_42/15:35:07.526 to 2017_42/16:25:47.526	-30.3034	-7.8285	-2.2974	
		0.303034	0.078285	0.022974	
		0.002	-0.009	0.001