FM576

Looking at the Restart states from Rev 577 we have the following results for FM576.
FM576		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	Oct 07 2016 18:42:21.139	42105.728	42105.943	42105.905	0.21556	0.17714	0.03841	17.82%	-0.05%	
MMS2	Oct 07 2016 18:42:24.690	42105.633	42105.943	42105.903	0.31046	0.27071	0.03975	12.80%	-0.03%	
MMS3	Oct 07 2016 18:42:24.550	42106.264	42105.939	42105.919	-0.32475	-0.34461	0.01986	-6.12%	-8.60%	
MMS4	Oct 07 2016 18:42:20.005	42105.923	42105.942	42105.918	0.01990	-0.00475	0.02465			
Looking at Restart States from Rev 578 and 579 gave small SMA change results by about 10 m.  MMS1 was 0.048 m/s and 43% axial, MMS2 was 0.041 m/s and 45% axial, MMS3 was 0.035 m/s and 22% axial. These small DV values produce larger percentage error values.
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 except MMS3 for DVY.
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)	
MMS2_FR576	2016_280/15:04:36 to 2016_280/15:04:36	0.021	-0.0196	0.0276	
		0.002	0.002	0.002	
		-0.00021	-0.00025	-0.0002	
MMS3_FR576	2016_280/16:34:36 to 2016_280/16:34:36	-0.0304	0.0245	-0.0054	
		0.002	0.002	0.002	
		-0.0004	-0.0008	-0.0004	
MMS1_FR576	2016_280/19:34:36 to 2016_280/19:34:36	0.0054	0.021	0.0453	
		0.002	0.002	0.002	
		0.0002	0.00015	-0.0005