AR702

Looking at the Restart states from Rev 703 we have the following results for AR702.
AR702		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)			
MMS1	Feb 11 2017 07:42:21.865	42109.924	44916.632	44918.106	2806.708	2808.182	-1.47435	-0.05%	0.02%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)		
MMS1	Feb 11 2017 07:42:21.865	1433.298	1578.958	1579.035	145.65998	145.73772	-0.07774	-4.66		
 
MMS1 was 31.19 m/s using 20.956 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 MMS1 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)	
MMS1_AR702	2017_40/15:49:18.747 to 2017_40/16:39:38.747	-30.1744	-7.6429	-2.1374	
		0.30174	0.076429	0.021374	
		0.007356	-0.006646	0.00476