FR1475

Looking at the Restart states from Rev 1476 we have the following results for FR1475
FR1475		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	Nov 22 2023 21:02:08	97744.024	97642.876	97642.912	-101.148	-101.112	-0.036	0.035%	0.287%	
MMS2	Nov 22 2023 21:04:46	97746.702	97668.239	97668.202	-78.463	-78.500	0.037	-0.048%	0.247%	
MMS3	Nov 22 2023 21:13:04	97751.469	97809.014	97809.097	57.545	57.628	-0.083	-0.144%	0.225%	
MMS4	Nov 22 2023 21:09:16	97749.136	97749.136	97749.160	0.000	0.024	-0.024			
 
MMS1 was 1.1399 m/s (net delta-v) and 41.59% axial, MMS2 was 0.5659 m/s and 39.79% axial, and MMS3 was 0.8094 m/s and 24.62% 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 MMS1 DVX and MMS2 DVX and 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_FR1475	2023_324/17:56:12 to 2023_324/17:57:22		-0.7781	0.1216	-0.1992	
		0.01	0.01	0.01	
		0.009136	-0.0003262	0.001876	
MMS1_FR1475	2023_324/19:31:12 to 2023_324/19:33:22		0.5129	-0.5151	-0.8815	
		0.01	0.01	0.01	
		0.01372	0.0008575	0.001992	
MMS2_FR1475	2023_324/22:56:12 to 2023_324/22:57:12		0.4901	0.1699	-0.2202	
		0.01	0.01	0.01	
		0.02725	0.02589	-0.003376