FM251

Looking at the Restart states from Rev 322 we have the following results for FM251. 

FM251		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	Nov 19 2015 08:12:02.139	42109.799	42106.628	42106.622	-3.171	-3.178	0.00675	-0.21%	
MMS2	Nov 19 2015 08:12:13.665	42109.785	42112.252	42112.248	2.467	2.462	0.00458	0.19%	
MMS3	Nov 19 2015 08:12:00.503	42109.791	42109.791	42109.794	0.000	0.002	-0.00243		
MMS4	Nov 19 2015 08:12:06.244	42109.771	42111.104	42111.108	1.334	1.337	-0.00356	-0.27%	

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 maneuver planning requirements for 1/ 2 orbit predictions for FM251
•	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 Restart states at 2015-320/22:51 (~1.5 orbits prior to the maneuver for FM251) vs the definitive GEONS state at the time of the maneuver.
The predicted velocity differences at the time of each maneuver are less than the greater of 1% of the delta-V or 10 mm/s for the first maneuver with significant margin.
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_FM251	322/11:35:35--322/11:36:15	-0.323348	-0.123663	0.199604	
		0.01	0.01	0.01	
		0.0005	0.0005	0.0005	
MMS4_FM251	322/13:10:35--322/13:10:45	0.02228	0.084641	0.138127	
		0.01	0.01	0.01	
		0.001	0.0014	0.0005	
MMS2_FM251	322/14:45:35--322/14:46:05	-0.107272	0.260315	0.336785	
		0.01	0.01	0.01	
		0.0006	0.001	0.0004	

All FM251 and FM252 maneuvers were planned using predicted ephemeris files based on GEONS post-perigee RST vectors @ 2015-319/22:36, one day prior to the CAM, which was held the prior day and final maneuver plans had to be prepared prior to the CAM.  Note that these predictions start 2+ orbits prior to FM251 and 3+ orbits prior to FM252.