FR981

Looking at the Restart states from Rev 982 we have the following results for FR981
FR981		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	Feb 24 2019 13:40:41.915	97372.018	97372.017	97372.008	0.000	-0.010	0.00986		
MMS2	Feb 24 2019 13:38:41.197	97366.399	97372.035	97372.040	5.636	5.641	-0.00468	-0.083%	
MMS3	Feb 24 2019 13:45:38.645	97365.423	97372.043	97372.099	6.620	6.676	-0.05638	-0.852%	
MMS4	Feb 24 2019 13:41:41.782	97385.258	97372.038	97372.079	-13.220	-13.179	-0.04113	0.311%	
 
MMS2 was 0.235 m/s (net delta-v) and 41.76% axial, MMS3 was 0.304 m/s and 41.37% axial, and MMS4 was 0.944 m/s and 45.27% 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 DVY for MMS2
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)	
MMS2_FR981	2019_51/10:39:07 to 2019_51/10:39:37	0.0832	-0.2195	0.0014	
		0.002	0.002195	0.002	
		-0.0008651	0.004961	-0.001075	
MMS3_FR981	2019_51/12:29:07 to 2019_51/12:29:37	0.1275	-0.275	-0.0074	
		0.002	0.00275	0.002	
		0.0006502	-0.001713	-0.0009703	
MMS4_FR981	2019_51/14:37:37 to 2019_51/14:39:37	-0.2913	0.8967	-0.0109	
		0.002913	0.008967	0.002	
		0.0006589	0.0008045	-0.0003064