FM504

Looking at the Restart states from Rev 505 we have the following results for FM504.
FM504		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	Jul 28 2016 03:05:54.534	42104.979	42104.041	42104.057	-0.93765	-0.92225	-0.01540	1.64%	0.42%	
MMS2	Jul 28 2016 03:06:01.135	42104.961	42107.473	42107.490	2.51180	2.52917	-0.01737	-0.69%	0.02%	
MMS3	Jul 28 2016 03:05:31.321	42105.003	42105.003	42105.030	0.00000	0.02669	-0.02669			
MMS4	Jul 28 2016 03:05:31.913	42104.995	42104.127	42104.146	-0.86795	-0.84933	-0.01863	2.15%	0.25%	

MMS1 was about 0.33 m/sec and equally radial and axial; MMS2 was about 0.81 m/s and mostly radial; MMS4 was about 0.18 m/s and more axial than radial.
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_FM504	2016_209/06:56:11 to 2016_209/06:56:31	-0.0967	0.0832	-0.1256	
		0.01	0.01	0.01	
		-0.00015	-0.0018	-0.0007	
MMS1_FM504	2016_209/08:11:11 to 2016_209/08:12:01	-0.1774	0.1803	-0.211	
		0.01	0.01	0.01	
		0.00025	-0.0018	-0.00052	
MMS2_FM504	2016_209/09:26:11 to 2016_209/09:27:31	0.6675	-0.3301	0.3238	
		0.01	0.01	0.01	
		0.00057	-0.0015	-0.00035