FM1683

Looking at the Restart states from Rev 1684 we have the following results for FM1683
FM1683		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 23 2025 07:38:59	97830.624	97821.807	97821.889	-8.817	-8.735	-0.082	0.933%	-0.072%	
MMS2	Nov 23 2025 07:39:26	97821.866	97821.838	97821.878	-0.028	0.011	-0.040	 		
MMS3	Nov 23 2025 07:39:32	97833.470	97821.971	97821.855	-11.499	-11.615	0.116	-1.008%	-0.349%	
MMS4	Nov 23 2025 07:38:59	97839.637	97821.981	97821.868	-17.656	-17.770	0.114	-0.643%	1.571%	
 
MMS1 was 0.67822 m/s (net delta-v) and 20.04% axial, MMS3 was 0.29921 m/s and 37.16% axial, and MMS4 was 1.24543 m/s and 13.59% 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 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_FM1683	2025_323/05:24:7 to 2025_323/05:24:37		-0.237	0.0334	-0.1572	
		0.00237	0.002	0.002	
		0.003527	-0.001875	-0.003546	
MMS4_FM1683	2025_323/16:47:47 to 2025_323/16:49:37		-1.2045	0.2252	-0.1047	
		0.012045	0.002252	0.002	
		0.000354	-0.0006071	-0.0004748	
MMS3_FM1683	2025_323/18:38:37 to 2025_323/18:39:37		-0.6465	0.1128	-0.1218	
		0.006465	0.002	0.002	
		0.001561	-0.0006002	-0.001453