FR1053

Looking at the Restart states from Rev 1055 we have the following results for FR1053
FR1053		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)		
MMS1	Nov 07 2019 06:37:03.035	97396.275	97399.058	97399.105	2.783	2.830	-0.04656	-1.673%	
MMS2	Nov 07 2019 06:36:59.268	97399.077	97399.075	97399.093	-0.002	0.016	-0.01769		
MMS3	Nov 07 2019 06:37:09.589	97392.633	97399.120	97399.173	6.486	6.540	-0.05325	-0.821%	
MMS4	Nov 07 2019 06:37:15.626	97391.278	97399.024	97399.021	7.747	7.743	0.00318	0.041%	
 
MMS1 was 0.137 m/s (net delta-v) and 26.25% axial, MMS3 was 0.481 m/s and 22.87% axial, and MMS4 was 0.759 m/s and 19.78% axial.

The Table below provides the following information:
•	The start and end times and planned maneuver 
•	Total delta-V (DeltaV_X, DeltaV_Y, and DeltaV_Z) for the first maneuver extracted from the DVTABLE files, 
•	The associated predicted velocity maneuver planning requirement for 1 and 2 orbit predictions (DeltaV_X Req, DeltaV_Y Req, and DeltaV_Z Req)
•	The difference between the predicted velocity and the GEONS definitive velocity at the start time of the first maneuver (Diff_V_X, Diff_V_Y, and Diff_V_Z).Planned maneuver total delta-V values based on the associated DVTABLEs  
As shown in the table below, all maneuvering spacecraft meet the requirement except MMS1 DVY.

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)	
MMS3_FR1053	2019_304/01:03:57 to 2019_304/01:04:37	0.2902	-0.2811	-0.2594	
		0.002902	0.002811	0.002594	
		0.0001235	-0.0014275	-0.0002610	
MMS4_FR1053	2019_304/02:53:27 to 2019_304/02:54:37	0.6119	-0.4471	-0.0313	
		0.006119	0.004471	0.002	
		0.0015149	-0.0019635	0.0003788	
MMS1_FR1053	2019_304/4:44:27 to 2019_304/4:44:37	0.1308	0.0085	-0.0396	
		0.002594	0.002	0.002	
		0.0004700	-0.0021738	-0.0001121