AR1625

Looking at the Restart states from Rev 1562 we have the following results for AR1625
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)		
MMS4	May 07 2025 01:02:10	97578.986	97461.719	97461.370	-117.267	-117.616	0.34884	-0.297%	
 
MMS4 was 0.41503 m/s and 0.41% 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)	
MMS4_AR1625	2025_121/18:51:23.541 to 2025_121/18:52:3.541		0.1994	0.3416		0.1257	
		0.01	0.01	0.01	
		-0.2813	0.064941		0.1169