FM848

Looking at the Restart states from Rev 849 we have the following results for FM848.
FM848		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	Plane change error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Feb 11 2018 02:56:29.637	84262.846	84262.800	84262.783	-0.046	-0.063	0.01690			
MMS2	Feb 11 2018 02:56:23.723	84263.748	84262.843	84262.840	-0.906	-0.908	0.00244	-0.269%	-1.645%	
MMS3	Feb 11 2018 02:56:23.449	84262.450	84262.801	84262.788	0.351	0.338	0.01345	3.832%	-2.301%	
MMS4	Feb 11 2018 02:56:40.688	84257.722	84262.776	84262.773	5.054	5.051	0.00384	0.076%	14.940%	
 
MMS2 was 0.11 m/s (net delta-v) and 30.41% axial, MMS3 was 0.054 m/s and 48.00% axial, and MMS4 was 0.165 m/s and 25.51% axial.
Small plane change (especially MMS4) and small SMA changes (MMS2 and MMS3) lead to large % errors.  

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 MMS2 DVZ
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_FM848	2018_38/16:09:27 to 2018_38/16:09:37	0.0468	-0.157	-0.0209	
		0.002	0.002	0.002	
		0.0003976	0.00149	0.0001695	
MMS3_FM848	2018_39/02:14:27 to 2018_39/02:14:37	0.0081	-0.0462	0.0252	
		0.002	0.002	0.002	
		-0.0002557	0.001757	-0.0001989	
MMS2_FM848	2018_39/04:04:27 to 2018_39/04:04:37	-0.0493	-0.1022	0.0067	
		0.002	0.002	0.002	
		-0.0001210	0.00155	-0.03418