FR882

Looking at the Restart states from Rev 883 we have the following results for FR882
FR882		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 17 2018 20:53:34.195	84243.999	84251.991	84252.020	7.992	8.021	-0.02888	-0.361%	0.938%	
MMS2	May 17 2018 20:53:22.342	84244.048	84244.048	84244.088	0.000	0.040	-0.04021			
MMS3	May 17 2018 20:53:27.208	84244.019	84240.338	84240.437	-3.681	-3.582	-0.09919	2.695%	0.545%	
MMS4	May 17 2018 20:53:18.835	84244.033	84235.267	84235.275	-8.767	-8.758	-0.00826	0.094%	0.515%	
 
MMS1 was 0.30m/s (net delta-v) and 0.38% axial, MMS3 was 0.18 m/s and 67.86% axial, and MMS4 was 0.12 m/s and 9.19% axial.
MMS1 and MMS4 were mostly radial, while MMS3 was mostly 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 except MMS4 DVX  
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_FR882	2018_136/02:15:52 to 2018_136/02:16:42	-0.30185	-0.00033	0.010676	
		0.01	0.01	0.01	
		0.005056	0.007925	-0.0002199	
MMS3_FR882	2018_136/03:50:52 to 2018_136/03:51:52	-0.04924	-0.087296	0.15682	
		0.01	0.01	0.01	
		-0.00589	0.005709	-0.001233	
MMS4_FR882	2018_136/05:25:52 to 2018_136/05:26:22	-0.015833	-0.10212	-0.052728	
		0.01	0.01	0.01	
		-0.01385	0.009423	-0.001434