AR729

Looking at the Restart states from Rev 731 we have the following results for AR729.
AR729		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS4	Mar 20 2017 22:41:28.370	60126.777	65389.155	65391.393	5262.379	5264.616	-2.23787	-0.043%	
		Period (min)	Period (min)	Period (min)	Period (min)	Per. (min)	Per. (min)	P-OD Per. (secs)	
MMS4	Mar 20 2017 22:41:28.370	2445.466	2773.437	2773.579	327.971	328.114	-0.14238	-8.54	
 
MMS4 was 28.7 m/s (net delta-v) using 17.42 kg
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 p lanning 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, MMS4 meets 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)	
MMS4_AR729	2017_77/00:58:5.459 to 2017_77/01:45:25.459	-27.503	-8.1008	-1.8479	
		0.27503	0.081008	0.018479	
		-0.06988	0.02425	0.01665