FR1223

Looking at the Restart states from Rev 1224 we have the following results for FR1223
FR1223		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	Jun 21 2021 01:07:22	97396.236	97390.909	97390.892	-5.328	-5.345	0.017	-0.318%	0.763%	
MMS2	Jun 21 2021 01:07:26	97390.932	97390.946	97390.918	0.014	-0.014	0.028			
MMS3	Jun 21 2021 01:07:51	97386.824	97390.914	97390.935	4.090	4.111	-0.022	-0.527%	0.294%	
MMS4	Jun 21 2021 01:07:53	97387.297	97390.923	97390.967	3.626	3.670	-0.044	-1.223%	0.382%	
 
MMS1 was 0.207 m/s (net delta-v) and 48.19% axial, MMS3 was 0.246 m/s and 14.76% axial, and MMS4 was 0.271 m/s and 55.29% 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 meet the requirement except MMS4 DVY and DVX.

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_FR1223	2021_167/16:58:57 to 2021_167/16:59:37		0.1438	-0.1536	0.1676	
		0.002	0.002	0.002	
		-4.409E-05	0.002237	0.002172	
MMS3_FR1223	2021_167/18:49:17 to 2021_167/18:49:37	0.0087	-0.2162	-0.121	
		0.002	0.002162	0.002	
		-0.0001844	0.00013	-4.898E-06	
MMS1_FR1223	2021_167/20:39:07 to 2021_167/20:39:37	-0.0866	-0.165	0.0928	
		0.002	0.002	0.002	
		-9.451E-06	2.893E-05	0.0001084