FR279

Looking at the Restart states from Rev 280 we have the following results for FR279.
The maneuvers for MMS4 did not take place until Rev 282/283.

FR279		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Dec 17 2015 05:06:54.936	42106.824	42100.559	42100.546	-6.265	-6.277	0.01265	-0.20%	
MMS2	Dec 17 2015 05:06:51.888	42106.820	42100.513	42100.495	-6.307	-6.324	0.01724	-0.27%	
MMS3	Dec 17 2015 05:06:47.465	42106.815	42106.815	42106.830	0.000	0.014	-0.01441		

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_FR279	350/11:30:35-350/11:33:05	0.41868	-1.1483	0.32865	
		0.01	0.011483	0.01	
		0.0003	0.0003	0.0002	
MMS2_FR279	350/10:15:35-350/10:16:55	-0.1218	-0.72633	0.15086	
		0.01	0.01	0.01	
		0.0002	0.0005	0.0001