FR202

Looking at the Restart states from Rev 203 we have the following results for FR202. 

FR202		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	Oct 01 2015 13:33:30.598	42111.861	42120.530	42120.606	8.668	8.745	-0.07630	-0.88%	
MMS2	Oct 01 2015 13:32:45.716	42111.823	42106.402	42106.480	-5.421	-5.342	-0.07807	1.44%	
MMS3	Oct 01 2015 13:32:51.625	42111.855	42086.422	42086.466	-25.433	-25.389	-0.04372	0.17%	
MMS4	Oct 01 2015 13:34:04.540	42111.750	42111.749	42111.815	-0.001	0.065	-0.06635		

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.
The predicted velocity meets all requirements 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)	
MMS2_FR202	273/04:20:35- 273/04:23:25	1.057043	-0.768393	0.773005	
		0.010	0.010	0.010	
		0.005	0.004	0.002	
MMS1_FR202	273/05:55:35– 273/06:01:15	2.459344	-0.175993	-2.053298	
		0.024	0.010	0.020	
		0.001	0.001	0.001	
MMS3_FR202	273/16:05:35- 273/16:10:35	-2.184484	-2.67493	-0.962097	
		0.021	0.026	0.010	
		0.002	0.001	0.001	

All FR202 and FR203 maneuvers were planned using predicted ephemeris files based on GEONS post-perigee RST vectors @ 2015-271/04:41, one day prior to the CAM.  Note that these predictions start 2+ orbits prior to FR202 because the FR202 maneuvers started only a couple of hours post-perigee,  CAM was held the prior day, and final maneuver plans had to be prepared prior to the CAM.