FM620

Looking at the Restart states from Rev 621 we have the following results for FM620.
FM620		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	Nov 20 2016 13:35:24.214	42105.035	42102.942	42102.927	-2.09388	-2.10852	0.01464	-0.70%	0.64%	
MMS3 was 0.27 m/s and 23.5% axial. 
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 planning 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 maneuvering spacecraft meet the requirement.
Maneuver ID	Timespan0	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_FM620	2016_324/15:06:11 to 2016_324/15:06:31	-0.2622	0.0633	-0.0559	
		0.01	0.01	0.01	
		-0.0002284	-0.0018720	-0.0005203