FR1434

Looking at the Restart states from Rev 1435 we have the following results for FR1434
FR1434		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	Jul 02 2023 05:10:37	97340.016	97340.045	97340.021	0.029	0.005	0.024	 		
MMS2	Jul 02 2023 05:10:19	97350.859	97340.033	97339.966	-10.826	-10.893	0.067	-0.618%	0.863%	
MMS3	Jul 02 2023 05:10:32	97331.374	97340.010	97339.965	8.636	8.591	0.045	0.520%	0.439%	
MMS4	Jul 02 2023 05:10:44	97337.446	97340.037	97339.993	2.591	2.547	0.044	1.711%	0.547%	
 
MMS2 was 0.2274 m/s (net delta-v) and 16.35% axial, MMS3 was 0.1833 m/s and 27.20% axial, and MMS4 was 0.14745 m/s and 36.03% 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, most do not 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_FR1434	2023_178/08:59:27 to 2023_178/08:59:37		0.0566	-0.174	-0.0013	
		0.002	0.002	0.002	
		-0.0003728	-0.01014	0.008512	
MMS4_FR1434	2023_178/15:54:27 to 2023_178/15:54:37		-0.0209	-0.0936	-0.1121	
		0.002	0.002	0.002	
		0.00654	-0.004151	-0.003247	
MMS2_FR1434	2023_178/19:44:17 to 2023_178/19:44:37		-0.2229	0.0101	0.0437	
		0.002229	0.002	0.002	
		-0.001105	0.008885	0.03976