FR1476

Looking at the Restart states from Rev 1477 we have the following results for FR1476
FR1476		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 26 2023 09:37:16	97562.015	97668.197	97668.269	106.182	106.254	-0.072	-0.068%	-1.154%	
MMS2	Nov 26 2023 09:37:21	97587.376	97668.200	97667.969	80.824	80.767	0.058	0.071%	2.071%	
MMS3	Nov 26 2023 09:37:18	97727.958	97668.209	97668.174	-59.750	-59.784	0.034	-0.058%	-0.030%	
MMS4	Nov 26 2023 09:36:51	97668.171	97668.171	97668.175	0.000	0.005	-0.005			
 
MMS1 was 4.2144 m/s (net delta-v) and 29.50% axial, MMS2 was 2.6920 m/s and 33.73% axial, and MMS3 was 1.6831 m/s and 39.19% 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 

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_FR1476	2023_326/03:31:37 to 2023_326/03:34:37			-1.277	0.3699	1.0344	
		0.01277	0.003699	0.010344	
		-0.00214	0.001115	0.000682	
MMS2_FR1476	2023_326/07:20:37 to 2023_326/07:24:37			2.3461	-0.3283	-1.2759	
		0.023461	0.003283	0.012759	
		0.003297	0.0004674	-0.001832	
MMS1_FR1476	2023_326/09:08:27 to 2023_326/09:14:37	3.7074	-0.8334	-1.8254	
		0.03707	0.008334	0.018254	
		0.004051	-0.002251	-0.003282