AR1105

Looking at the restart states from Rev 1106 we have the following results for AR1105
AR1105		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	05/07/2020 10:34:52	97345.670	97154.880	97154.806	-190.790	-190.863	0.07331	-0.038%	
MMS2	05/07/2020 10:34:54	97345.711	97154.870	97154.600	-190.841	-191.111	0.27021	-0.142%	
MMS3	05/07/2020 10:35:18	97345.764	97154.957	97154.686	-190.807	-191.078	0.27081	-0.142%	
MMS4	05/07/2020 10:35:23	97345.756	97154.945	97154.906	-190.811	-190.850	0.03931	-0.021%	
 
MMS1 was 0.693 m/s (net delta-v) and 0.30% axial, MMS2 was 0.695m/s  and 0.52% axial, MMS3 was 0.693 m/s and 0.55% axial, and MMS4 was 0.694 m/s and 0.38% 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 

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_AR1105	2020_123/04:56:20 to 2020_123/04:57:30 	0.5207	0.4315	0.1487	
		0.01	0.01	0.01	
		0.1	-0.135	-0.025	
MMS2_AR1105	2020_123/04:56:20 to 2020_123/04:57:30 	0.5223	0.4318	0.1501	
		0.01	0.01	0.01	
		0.1	-0.144	-0.02	
MMS3_AR1105	2020_123/04:56:50 to 2020_123/04:57:50 	0.5195	0.4333	0.1493	
		0.01	0.01	0.01	
		0.1735	-0.2394	-0.02624	
MMS4_AR1105	2020_123/04:57:00 to 2020_123/04:58:00  	0.519	0.4339	0.1494	
		0.01	0.01	0.01	
		0.1922	-0.2388	-0.02628