FR1534

Looking at the Restart states from Rev 1535 we have the following results for FR1534
FR1534		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 17 2024 16:35:07	97760.911	97755.730	97755.780	-5.181	-5.131	-0.050	0.965%	0.324%	
MMS2	Jun 17 2024 16:37:21	97755.849	97755.803	97755.844	-0.046	-0.005	-0.041	 		
MMS3	Jun 17 2024 16:36:14	97763.714	97755.759	97755.874	-7.955	-7.840	-0.115	1.445%	-6.162%	
MMS4	Jun 17 2024 16:38:28	97752.560	97755.799	97755.840	3.239	3.280	-0.041	-1.253%	-0.424%	
 
MMS1 was 1.4447 m/s (net delta-v) and 38.24% axial, MMS3 was 1.042 m/s and 35.60% axial, and MMS4 was 0.6682 m/s and 27.98% 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)	
MMS4_FR1534	2024_165/19:13:37 to 2024_165/19:14:37		0.3743	-0.4054	-0.3732	
		0.003743	0.004054	0.003732	
		-0.001138	-0.0008468	0.0003568	
MMS3_FR1534	2024_165/21:02:57 to 2024_165/21:04:37		-0.7547	0.384	0.605	
		0.007547	0.00384	0.00605	
		0.0006349	0.0008261	-0.0002957	
MMS`_FR1534	2024_165/22:52:07 to 2024_165/22:54:37		-1.0179	0.4954	0.8963	
		0.010179	0.004954	0.008963	
		-0.001838	0.0007766	0.001178