FI987

Looking at the Restart states from Rev 988 we have the following results for FI987
FI987		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	Mar 17 2019 14:12:24.036	97416.558	97442.687	97442.807	26.129	26.250	-0.12083	-0.462%	
MMS2	Mar 17 2019 14:12:23.820	97389.072	97442.696	97442.761	53.624	53.689	-0.06444	-0.120%	
MMS3	Mar 17 2019 14:12:14.829	97482.347	97442.691	97442.784	-39.656	-39.564	-0.09259	0.233%	
MMS4	Mar 17 2019 14:12:09.871	97442.692	97442.691	97442.715	0.000	0.024	-0.02381		
 
MMS1 was 1.318 m/s (net delta-v) and 34.23% axial, MMS2 was 2.999 m/s and 33.19% axial, and MMS3 was 3.165 m/s and 32.25% 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 .
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_FI987	2019_72/12:32:37 to 2019_72/12:34:37	0.4479	-1.2379	0.0231	
		0.004479	0.012379	0.002	
		0.00008243	0.000201	0.0002429	
MMS2_FI987	2019_72/14:20:17 to 2019_72/14:24:37	1.2335	-2.7332	0.0028	
		0.012335	0.027332	0.002	
		0.00009627	0.00006658	0.0002063	
MMS3_FI987	2019_72/16:10:07 to 2019_72/16:14:37	-1.1	2.9682	0.0748	
		0.011	0.029682	0.002	
		-0.00005765	0.00002085	0.0002263