FR280

Looking at the Restart states from Rev 281 we have the following results for FR280.
The maneuvers for MMS4 did not take place until Rev 282/283.

FR280		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 18 2015 05:00:02.999	42100.677	42106.911	42106.924	6.235	6.247	-0.01241	-0.20%	
MMS2	Dec 18 2015 05:00:26.038	42100.624	42106.903	42106.910	6.279	6.286	-0.00743	-0.12%	

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_FR280	351/06:12:00-351/06:14:00	0.68381	0.13331	-0.64471	
		0.0068381	0.002	0.0064471	
		0.001	0.0015	0.0005	
MMS2_FR280	351/04:37:00-351/04:39:00	0.077218	-1.0854	-1.0677	
		0.002	0.010854	0.010677	
		0.0005	0.0007	0.0003