FM1451

Looking at the Restart states from Rev 1452 we have the following results for FM1451
FM1451		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	Aug 30 2023 17:54:24	97548.564	97548.564	97548.622	0.000	0.058	-0.058			
MMS2	Aug 30 2023 17:49:44	97548.412	97437.544	97437.410	-110.869	-111.003	0.134	-0.121%	1.799%	
MMS3	Aug 30 2023 17:48:16	97548.483	97393.901	97393.943	-154.582	-154.540	-0.042	0.027%	-0.152%	
MMS4	Aug 30 2023 17:51:15	97548.415	97462.929	97462.876	-85.486	-85.539	0.053	-0.062%	0.030%	
 
MMS2 was 1.233 m/s (net delta-v) and 33.16% axial, MMS3 was 1.821 m/s and 20.50% axial, and MMS4 was 1.350 m/s and 39.48% 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 MMS2 DVX and MMS3 DVY and DVZ.

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_FM1451	2023_240/15:41:12 to 2023_240/15:43:32	1.0404	0.8005	-0.312	
		0.010404	0.01	0.01	
		0.007468	0.002354	-0.005177	
MMS2_FM1451	2023_240/17:01:12 to 2023_240/17:03:02
	1.1051	0.4747	-0.2602	
		0.011051	0.01	0.01	
		0.01581	0.002907	-0.009769	
MMS3_FM1451	2023_240/18:26:12 to 2023_240/18:29:02	1.5638	0.927	0.0597	
		0.015638	0.01	0.01	
		-0.001525	0.0104	-0.01514