AR1638

Looking at the Restart states from Rev 1640 we have the following results for AR1638
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	Jun 21 2025 14:22:43	97365.010	97489.455	97489.392	124.446	124.383	0.06267	0.050%	
 
MMS4 was 0.4553 m/s and 0.52% 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_AR1638	2025_167/7:46:10.382 to 2025_167/7:46:50.382		-0.2269	-0.3707	-0.1333	
		0.002269	0.003707	0.002	
		-0.1893	0.04936	0.08369