FM621

Looking at the Restart states from Rev 622 we have the following results for FM621.
FM622		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				42103.311						
MMS2				42103.283						
MMS3	Nov 21 2016 13:28:19.905	42102.307	42103.288	42103.292	0.98167	0.98490	-0.00323	-0.33%	0.17%	
MMS4				42103.297						
 MMS1 was 0.36 m/s and 3% 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	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_FM621	2016_325/12:14:06 to 2016_325/12:14:36	0.1766	0.2726	0.1449	
		0.002	0.002	0.002	
		-0.0002572	-0.0008106	-0.0002949