AR1539

Looking at the Restart states from Rev 1541 we have the following results for AR1539
AR1539		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)		
MMS1	Jul 08 2024 19:39:07.463	97814.015	97758.636	97758.789	-55.379	-55.227	-0.15214	0.275%	
MMS2	Jul 08 2024 19:42:16.184	97814.011	97766.227	97766.950	-47.783	-47.061	-0.72269	1.512%	
MMS3	Jul 08 2024 19:41:08.527	97814.073	97766.018	97766.407	-48.054	-47.665	-0.38888	0.809%	
MMS4	Jul 08 2024 19:53:03.097	97813.967	97848.959	97849.044	34.992	35.077	-0.08509	-0.243%	
 
MMS1 was 0.13647 m/s (net delta-v) and 0.14% axial, MMS2 was 0.11883 m/s and 0.17% axial, MMS3 was 0.1179 m/s and 0.50% axial, and MMS4 was 0.087397 m/s and 0.00% 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)	
MMS1_AR1539	2024_185/12:55:30 to 2024_185/12:55:50		0.0651	0.112	0.0426	
		0.01	0.01	0.01	
		0.1584	-0.03836	-0.064	
MMS2_AR1539	2024_185/12:57:50 to 2024_185/12:58:10		0.0559	0.0969	0.0366	
		0.01	0.01	0.01	
		-0.08139	-0.07098	-0.08632	
MMS3_AR1539	2024_185/12:56:40 to 2024_185/12:57:00		0.0565	0.0972	0.0369	
		0.01	0.01	0.01	
		0.04054	-0.08079	-0.1439	
MMS4_AR1539	2024_185/12:59:00 to 2024_185/12:59:10		-0.0409	-0.0708	-0.0269	
		0.01	0.01	0.01	
		-0.03286	0.03737	0.05018