FM1627

Looking at the Restart states from Rev 1629 we have the following results for FM1627
FM1627		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	May 13 2025 23:35:29	97529.829	97523.849	97523.890	-5.979	-5.938	-0.041	0.682%	0.627%	
MMS2	May 13 2025 23:35:37	97523.017	97523.680	97523.712	0.663	0.695	-0.032	-4.820%	-1.412%	
MMS3	May 13 2025 23:35:40	97528.316	97523.838	97523.819	-4.478	-4.496	0.019	-0.416%	-0.288%	
MMS4	May 14 2025 01:10:59	97393.407	97393.359	97393.363	-0.049	-0.045	-0.004	 		
 
MMS1 was 0.3550 m/s (net delta-v) and 71.68% axial, MMS2 was 0.2094 m/s and 37.97% axial, and MMS3 was 0.1908 m/s and 17.43% axial.
Larger % errors on MMS2 due to maneuver being so much smaller than the other two.
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.

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)	
MMS3_FM1627	2025_127/05:34:17 to 2025_127/05:34:37		-0.0255	-0.1591	-0.0994	
		0.002	0.002	0.002	
		0.007514	0.02662	0.1052	
MMS2_FM1627	2025_127/09:19:17 to 2025_127/09:19:37		0.1793	-0.0176	0.1038	
		0.002	0.002	0.002	
		0.002226	-0.0006308	0.016	
MMS1_FM1627	2025_127/12:48:17 to 2025_127/12:49:37		0.0671	0.2101	-0.2804	
		0.002	0.002101	0.002804	
		-0.0008711	-0.01488	0.0192