FR1533

Looking at the Restart states from Rev 1534 we have the following results for FR1533
FR1533		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 14 2024 04:06:21	97784.197	97789.301	97789.212	5.104	5.015	0.089	1.740%	0.783%	
MMS2	Jun 14 2024 04:06:22	97784.150	97784.150	97784.153	0.000	0.004	-0.004	 		
MMS3	Jun 14 2024 04:06:53	97784.193	97792.083	97792.030	7.890	7.837	0.053	0.672%	1.597%	
MMS4	Jun 14 2024 04:06:32	97784.153	97780.855	97780.867	-3.299	-3.287	-0.012	0.370%	0.852%	
 
MMS1 was 0.7726 m/s (net delta-v) and 43.41% axial, MMS3 was 0.3504 m/s and 48.52% axial, and MMS4 was 0.3591 m/s and 15.84% 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, MMS3 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)	
MMS1_FR1533	2024_163/23:21:12 to 2024_163/23:22:52		-0.4363	-0.3111	-0.5574	
		0.01	0.01	0.01	
		-0.01443	-0.001269	0.005115	
MMS4_FR1533	2024_164/00:56:12 to 2024_164/00:56:42		0.1409	0.325	0.0596	
		0.01	0.01	0.01	
		-0.005987	-0.001111	0.0006479	
MMS3_FR1533	2024_164/04:06:12 to 2024_164/04:07:02		-0.1843	-0.0939	-0.2836	
		0.01	0.01	0.01	
		-0.02505	-0.004162	-0.002559