FR1614 and FR1615 MMS1

Looking at the Restart states from Revs 1615 and 1616 we have the following results for MMS1
		NoBurn	Plan	OD	Plan-
NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS1	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
FR1614	Mar 25 2025 19:16:02	97650.472	97670.994	97670.994	20.522	20.522	0.001	0.003%	
FR1615	Mar 29 2025 07:41:29	97645.022	97632.704	97632.713	-12.318	-12.309	-0.009	0.072%	
 
MMS1 FR1614 was 0.6529 m/s (net delta-v) and 48.12% axial, FR1615 was 1.5952 m/s and 30.65% 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)	
MMS1_FR1614	2025_82/10:51:12 to 2025_82/10:52:42		0.0812	0.3088	0.5679	
		0.01	0.01	0.01	
		0.004745	-0.001918	-0.0004365	
MMS1_FR1615	2025_65/03:56:12 to 2025_65/04:00:12	1.2123	-0.5446	-0.8843	
		0.012123	0.005446	0.008843	
		0.001294	-0.0001227	-0.001101