FR554

Looking at the Restart states from Rev 555 we have the following results for FR554.
FR554		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										
MMS2	Sep 16 2016 21:09:39.472	42101.771	42102.880	42102.909	1.10920	1.13795	-0.02876	-2.59%	0.01%	
MMS3	Sep 16 2016 21:09:38.178	42101.865	42101.752	42101.770	-0.11270	-0.09491	-0.01779	15.79%	1.32%	
MMS4	Sep 16 2016 21:09:31.849	42101.846	42102.047	42102.052	0.20107	0.20642	-0.00535	-2.66%	0.42%	
MMS1 did not maneuver at all. Not even DH.  MMS2 was 0.08 m/s and 48% axial, MMS3 was 0.11 m/s and 52% axial, MMS4 was 0.13 m/s and 70% axial. The extremely small SMA change for MMS3 should be note when looking at the 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.
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_FR554	2016_259/02:16:11 to 2016_259/02:16:31	-0.0511	-0.0232	0.1213	
		0.01	0.01	0.01	
		0.000202	-0.001062	-0.0002744	
MMS2_FR554	2016_259/03:51:11 to 2016_259/03:51:21	0.0167	0.0338	0.0728	
		0.01	0.01	0.01	
		0.0003566	-0.001123	-0.0002708	
MMS3_FR554	2016_259/05:26:11 to 2016_259/05:26:21	0.0673	-0.0459	0.0744	
		0.01	0.01	0.016059	
		0.001309	-0.002472	-0.00079