FR1645

Looking at the Restart states from Rev 1646 we have the following results for FR1645
FR1645		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	Jul 12 2025 15:48:17	97610.263	97610.241	97610.211	-0.022	-0.052	0.031	 		
MMS2	Jul 12 2025 15:48:14	97629.278	97610.132	97610.164	-19.146	-19.114	-0.032	0.167%	-0.928%	
MMS3	Jul 12 2025 15:48:43	97620.053	97610.133	97610.052	-9.920	-10.001	0.081	-0.813%	1.616%	
MMS4	Jul 12 2025 15:48:48	97611.049	97610.287	97610.332	-0.762	-0.717	-0.045	5.911%	5.013%	
 
MMS2 was 0.6891 m/s (net delta-v) and 30.03% axial, MMS3 was 0.5173 m/s and 73.84% axial, and MMS4 was 0.3447 m/s and 36.65% axial.
Larger % errors on MMS4 due to maneuver being much smaller than the other two. There are some OD errors which most likely affect the results.

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.
Mnvr ID	Time Span	DeltaV_X (m/s)	DeltaV_X Req (m/s)	Diff_V_X (m/s)	DeltaV_Y (m/s)	DeltaV_Y Req (m/s)	Diff_V_Y (m/s)	DeltaV_Z (m/s)	DeltaV_Z Req (m/s)	Diff_V_Z (m/s)	
MMS4	2025_189/18:14:7 to 2025_189/18:14:37	0.1375	0.002	-1.314e-05	-0.2039	0.002039	-0.001356	-0.2468	0.002468	-0.001538	
MMS3	2025_189/20:02:47 to 2025_189/20:04:37	-0.0961	0.002	0.001312	0.0913	0.002	-0.001232	-0.5003	0.005003	-0.0008782	
MMS2	2025_189/21:53:37 to 2025_189/21:54:37	-0.5047	0.005047	-0.001727	-0.2789	0.002789	-0.0002152	-0.3774	0.003774	0.000384