FR1111

Looking at the Restart states from Rev 1112 we have the following results for FR1111
FR1111		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	05/24/2020 21:33:12	97213.692	97214.021	97213.937	0.329	0.245	0.08387	25.464%	11.698%	
MMS2	05/24/2020 21:33:13	97213.940	97213.900	97213.899	-0.040	-0.042	0.00118			
MMS3	05/24/2020 21:33:22	97218.200	97213.875	97213.806	-4.326	-4.395	0.06898	-1.595%	5.403%	
MMS4	05/24/2020 21:33:26	97218.949	97214.032	97213.953	-4.917	-4.996	0.07903	-1.607%	-10.706%	
 
MMS1 was 0.191 m/s (net delta-v) and 41.04% axial, MMS3 was 0.275 m/s and 20.06% axial, and MMS4 was 0.354 m/s and 31.21% axial.
The MMS1 SMA change was small compared to OD error.
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, only 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)	
MMS1_FR1111	2020_141/13:39:17 to 2020_141/13:39:37   	0.0557	0.1712	-0.0483	
		0.002	0.002	0.002	
		0.04197	0.135	-0.03902	
MMS3_FR1111	2020_141/21:4:17 to 2020_141/21:4:37  	-0.1008	0.2461	0.0359	
		0.002	0.002461	0.002	
		-0.08662	0.2135	0.03153	
MMS4_FR1111	2020_141/22:54:7 to 2020_141/22:54:37  	-0.1847	0.2933	-0.0186	
		0.002	0.002933	0.002	
		0.001812	0.001822	0.0001392