FM898

Looking at the Restart states from Rev 899 we have the following results for FM898
FM898		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	Jul 01 2018 22:31:54.276	84262.932	84262.891	84262.892	-0.041	-0.040	-0.00096			
MMS2	Jul 01 2018 22:31:52.043	84262.025	84262.849	84262.849	0.824	0.825	-0.00029	-0.035%	4.000%	
MMS3	Jul 01 2018 22:32:21.617	84264.858	84262.855	84262.901	-2.003	-1.957	-0.04618	2.306%	-24.203%	
MMS4	Jul 01 2018 22:32:23.849	84262.127	84262.831	84262.853	0.704	0.727	-0.02240	-3.181%	0.933%	
 
MMS2 was 0.099 m/s (net delta-v) and 4.83% axial, MMS3 was 0.17 m/s and 18.35% axial, and MMS4 was 0.092 m/s and 7.69% axial.
MMS3 had very little plane change (more than a factor of 10 smaller than the other 2 MMS).

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)	
MMS3_FM898	2018_178/08:21:12 to 2018_178/08:21:22	0.075	0.0628	0.0256	
		0.002	0.002	0.002	
		-0.00007696	-0.0002608	0.000189	
MMS2_FM898	2018_178/09:56:12 to 2018_178/09:56:32	0.0543	0.1625	0.0221	
		0.002	0.002	0.002	
		-0.0001766	0.00002508	0.000688	
MMS4_FM898	2018_178/11:31:12 to 2018_178/11:31:22	0.0385	0.0787	0.037	
		0.002	0.002	0.002	
		-0.0001457	0.0002778	0.000223