FM1682

Looking at the Restart states from Rev 1683 we have the following results for FM1682
FM1682		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	Nov 19 2025 19:05:29	97844.805	97853.783	97853.754	8.978	8.949	0.029	0.322%	0.968%	
MMS2	Nov 19 2025 19:04:58	97844.978	97844.978	97844.987	0.000	0.009	-0.009	 		
MMS3	Nov 19 2025 19:05:29	97844.476	97856.455	97856.624	11.978	12.148	-0.170	-1.418%	1.010%	
MMS4	Nov 19 2025 19:06:24	97844.670	97862.682	97862.786	18.012	18.116	-0.104	-0.579%	0.513%	
 
MMS1 was 0.33444 m/s (net delta-v) and 74.43% axial, MMS3 was 0.215797 m/s and 53.02% axial, and MMS4 was 0.561268 m/s and 65.05% 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, MMS4 MVZ, MMS3 DVX 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)	
MMS1_FM1682	2025_321/16:31:12 to 2025_321/16:32:22		-0.0754	-0.2036	0.2619	
		0.01	0.01	0.01	
		0.01317	0.002829	0.005615	
MMS4_FM1682	2025_321/18:06:12 to 2025_321/18:08:02		-0.1827	-0.4073	0.3555	
		0.01	0.01	0.01	
		0.00567	-2.694E-05	0.02576	
MMS3_FM1682	2025_321/19:41:12 to 2025_321/19:41:52		-0.1027	-0.1544	0.1094	
		0.01	0.01	0.01	
		0.02321	0.002122	0.01483