FR1609

Looking at the Restart states from Rev 1610 we have the following results for FR1609
FR1609		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	Mar 08 2025 05:25:36	97602.699	97388.783	97388.566	-213.916	-214.133	0.217	-0.101%	0.665%	
MMS2	Mar 08 2025 05:39:28	97601.367	97684.193	97684.269	82.827	82.903	-0.076	-0.092%	-2.328%	
MMS3	Mar 08 2025 05:34:11	97601.477	97569.581	97569.625	-31.896	-31.852	-0.045	0.140%	0.363%	
MMS4	Mar 08 2025 07:51:20	97601.346	97601.346	97601.404	0.000	0.058	-0.058	 		
 
MMS1 was 2.6252 m/s (net delta-v) and 34.23% axial, MMS2 was 1.5327 m/s and 33.46% axial, and MMS3 was 0.5369 m/s and 60.28% 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 

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)	
MMS2_FR1609	2025_65/02:31:12 to 2025_65/02:33:32	-1.2813	-0.3792	-0.7488	
		0.012813	0.01	0.01	
		0.0007198	-0.0009967	-0.00006785	
MMS1_FR1609	2025_65/03:56:12 to 2025_65/04:00:12	2.4199	0.0606	1.0153	
		0.024199	0.01	0.010153	
		0.007622	-0.001373	0.003914	
MMS3_FR1609	2025_65/05:21:12 to 2025_65/05:22:52		0.3097	-0.2729	0.3399	
		0.01	0.01	0.01	
		0.005212	0.0016	0.001799