FR883

Looking at the Restart states from Rev 884 we have the following results for FR883
FR883		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	May 20 2018 16:30:08.243	84256.522	84248.544	84248.554	-7.977	-7.968	-0.00955	0.120%	7.690%	
MMS2	May 20 2018 16:30:09.430	84248.587	84248.537	84248.563	-0.050	-0.024	-0.02590			
MMS3	May 20 2018 16:30:38.421	84244.943	84248.610	84248.627	3.667	3.685	-0.01787	-0.487%	-0.395%	
MMS4	May 20 2018 16:30:43.958	84239.780	84248.520	84248.570	8.740	8.790	-0.05050	-0.578%	2.193%	
 
MMS1 was 0.33m/s (net delta-v) and 12.03% axial, MMS3 was 0.39 m/s and 0.77% axial, and MMS4 was 0.54 m/s and 24.16% axial.
MMS1 had a very small plane value (an order of magnitude less than MMS3 and MMS4).    
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)	
MMS1_FR883	2018_137/01:18:47 to 2018_137/01:19:37	-0.32663	-0.055422	-0.054171	
		0.0032663	0.002	0.002	
		7.677e-05	0.0003228	-0.0001432	
MMS4_FR883	2018_137/07:18:27 to 2018_137/07:19:37	-0.06122	-0.53651	-0.045253	
		0.002	0.005365	0.002	
		4.02e-05	9.375e-05	-0.0003163	
MMS3_FR883	2018_137/09:08:37 to 2018_137/09:09:37	-0.062839	-0.36006	-0.13289	
		0.002	0.0036006	0.002	
		4.618e-05	9.082e-05	-0.0003262