AR1146

Looking at the restart states from Rev 1147 we have the following results for AR1146
AR1146		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	 09/27/2020 16:42:48	97342.588	97577.790	97577.945	235.202	235.357	-0.15489	-0.066%	
MMS2	09/27/2020 16:42:58	97342.711	97577.763	97578.163	235.052	235.452	-0.39977	-0.170%	
MMS3	09/27/2020 16:43:18	97342.731	97577.783	97577.901	235.051	235.170	-0.11826	-0.050%	
MMS4	09/27/2020 16:43:32	97342.787	97577.857	97578.004	235.070	235.217	-0.14686	-0.062%	
 
MMS1 was 1.0086 m/s (net delta-v) and 0.45% axial, MMS2 was 1.0095 m/s and 0.55% axial, MMS3 was 1.008 m/s and 0.71% axial, and MMS4 was 1.0082 m/s and 0.61% 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, none of the maneuvering spacecraft meet the requirement as usual for apogee adjustments.

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_AR1146	2020_266/10:28:20 to 2020_266/10:29:50		-0.6619	-0.6873	-0.3258	
		0.01	0.01	0.01	
		-0.05191	0.05372	0.006858	
MMS2_AR1146	2020_266/10:28:30 to 2020_266/10:30:00		-0.6628	-0.6872	-0.3261	
		0.01	0.01	0.01	
		-0.04481	0.05474	0.005454	
MMS3_AR1146	2020_266/10:28:50 to 2020_266/10:30:20		-0.6608	-0.6878	-0.3259	
		0.01	0.01	0.01	
		0.04961	-0.0625	-0.00746	
MMS4_AR1146	2020_266/10:29:00 to 2020_266/10:30:30		-0.6608	-0.6877	-0.3259	
		0.01	0.01	0.01	
		0.03876	-0.0654	-0.02238