AR1672

Looking at the Restart states from Rev 1674 we have the following results for AR1672
AR1625		NoBurn	Plan	OD	Plan-
NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Oct 19 2025 01:05:55	97556.804	97890.574	97891.065	333.770	334.261	-0.49110	-0.147%	
MMS2	Oct 19 2025 01:05:38	97556.489	97890.570	97891.201	334.081	334.712	-0.63103	-0.189%	
MMS3	Oct 19 2025 01:06:04	97556.514	97890.585	97890.745	334.071	334.231	-0.16028	-0.048%	
MMS4	Oct 19 2025 01:06:36	97556.638	97890.574	97890.839	333.936	334.201	-0.26485	-0.079%	
 
MMS1 was 1.2639 m/s and 0.52% axial, MMS2 was 1.2639 m/s and 0.53% axial, MMS3 was 1.26459 m/s and 0.79% axial, MMS4 was 1.2637 m/s and 0.45% 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 do not meet the requirement, as usual for apogee adjustments.

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_AR1672	2025_286/18:01:40 to 2025_286/18:03:50		-0.6364	    -0.9735	-0.4914	
		0.006364	0.009735	0.004914	
		-0.2164	0.06119	0.07188	
MMS2_AR1672	2025_286/18:01:30 to 2025_286/18:03:40		-0.6335		-0.9752		-0.4924		
		0.006335	0.009752	0.004924	
		-0.2918	0.08464		0.1048	
MMS3_AR1672	2025_286/18:01:50 to 2025_286/18:04:00		-0.6364	-0.9746	-0.4915	
		0.006364	0.009746	0.004915	
		-0.2954	0.0853	0.11	
MMS4_AR1672	2025_286/18:02:30 to 2025_286/18:04:40		-0.6326	-0.9760	-0.4924		
		0.006326	0.00976	0.004924	
		-0.2925	0.08507	0.1077