FM1412

Looking at the Restart states from Rev 1413 we have the following results for FM1412
FM1412		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	Apr 16 2023 04:31:12	97554.526	97524.150	97523.937	-30.376	-30.589	0.213	-0.700%	-0.874%	
MMS2	Apr 16 2023 04:32:09	97554.468	97554.468	97554.526	0.000	0.057	-0.057			
MMS3	Apr 16 2023 04:31:02	97554.571	97528.684	97528.594	-25.887	-25.977	0.090	-0.347%	-0.336%	
MMS4	Apr 16 2023 04:29:24	97554.514	97487.969	97487.984	-66.545	-66.530	-0.015	0.023%	-0.566%	
 
MMS1 was 0.70297 m/s (net delta-v) and 45.77% axial, MMS3 was 0.42248 m/s and 44.56% axial, and MMS4 was 0.76998 m/s and 46.78% 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 MMS3 DVX and MMS1 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)	
MMS1_FM1412	2023_104/00:06:12 to 2023_104/00:07:42
	0.444	0.4843	-0.2294	
		0.01	0.01	0.01	
		-0.009223	0.001078	0.0121	
MMS3_FM1412	2023_104/01:41:12 to 2023_104/01:42:22
		0.4137	0.2971	-0.2188	
		0.01	0.01	0.01	
		-0.01547	0.0002769	0.00838	
MMS4_FM1412	2023_104/03:16:12 to 2023_104/03:18:2	0.7113	0.4222	-0.3996	
		0.01	0.01	0.01	
		-0.008307	0.001324	0.00602