FI807

Looking at the Restart states from Rev 808 we have the following results for FI807.
FI807		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Oct 18 2017 15:00:48.593	84189.644	84205.661	84205.660	16.016	16.016	0.00042	0.003%	
MMS2	Oct 18 2017 15:00:31.187	84205.795	84205.753	84205.754	-0.042	-0.041			
MMS3	Oct 18 2017 15:00:44.928	84228.617	84205.794	84205.761	-22.823	-22.856	0.03301	-0.145%	
MMS4	Oct 18 2017 15:01:01.453	84237.505	84205.731	84205.868	-31.774	-31.637	-0.13690	0.431%	
 
MMS1 was 2.58 m/s (net delta-v) and 4.96% axial, MMS3 was 2.63 m/s and 18.98% axial, and MMS4 was 3.58 m/s and 3.19% 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)	
MMS4_FI807	2017_288/01:49:07 to 2017_288/01:54:37	2.1783	2.5577	1.201	
		0.021783	0.025577	0.01201	
		-0.000007176	-0.00006184	0.0002629	
MMS1_FI807	2017_288/03:40:37 to 2017_288/03:44:37	-1.4671	-1.861	-1.0408	
		0.014671	0.01861	0.010408	
		-0.00006764	-0.00009593	0.0001875	
MMS3_FI807	2017_288/05:20:37 to 2017_288/05:24:37	1.2751	2.2337	0.552	
		0.012751	0.022337	0.00552	
		-0.0002323	-0.00007768	-0.000006702