FR694

Looking at the Restart states from Rev 695 we have the following results for FR694.
FR694		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	dSMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	Feb 02 2017 05:03:14.303	42106.396	42097.730	42097.746	-8.66596	-8.64906	-0.01690	0.19%	0.09%	
MMS2	Feb 02 2017 05:03:30.554	42106.409	42106.409	42106.453	-0.00001	0.04348	-0.04348			
MMS3	Feb 02 2017 05:03:34.669	42106.399	42112.076	42112.123	5.67752	5.72387	-0.04635	-0.82%	0.12%	
MMS4	Feb 02 2017 05:03:32.474	42106.414	42097.735	42097.746	-8.67924	-8.66735	-0.01189	0.14%	0.14%	

MMS1 was 1.53 m/s and 53.3% axial, MMS3 was 2.74 m/s and 65.4% axial, MMS4 was 2.97 m/s and 77.7% 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	Timespan0	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)	
MMS4_FR694	2017_32/09:16:12 to 2017_32/09:25:12	-0.3382	-2.0232	2.1782	
		0.01	0.020232	0.021782	
		-0.0008874	0.003952	0.000963	
MMS1_FR694	2017_32/10:51:12 to 2017_32/10:54:42	-0.9853	-0.8153	0.8627	
		0.01	0.01	0.01	
		-0.0009931	0.003732	0.000667	
MMS3_FR694	2017_32/12:26:12 to 2017_32/12:34:02	-1.1976	-0.6114	2.4181	
		0.011976	0.01	0.024181	
		-0.002777	0.005575	0.000496