FM1513

Looking at the Restart states from Rev 1514 we have the following results for FM1513
FM1513		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	Apr 04 2024 17:35:36	97900.839	97900.839	97900.858	0.000	0.019	-0.019			
MMS2	Apr 04 2024 17:35:02	97900.886	97889.898	97889.810	-10.988	-11.075	0.088	-0.799%	0.457%	
MMS3	Apr 04 2024 17:34:55	97900.791	97885.669	97885.624	-15.122	-15.167	0.045	-0.299%	1.231%	
MMS4	Apr 04 2024 17:34:22	97900.806	97874.895	97874.906	-25.911	-25.900	-0.012	0.045%	3.097%	
 
MMS2 was 0.32852 m/s (net delta-v) and 83.54% axial, MMS3 was 0.27074 m/s and 42.04% axial, and MMS4 was 0.41363 m/s and 18.15% 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)	
MMS4_FM1513	2024_093/09:11:12 to 2024_93/09:11:52		0.4037	0.0344	-0.0908	
		0.01	0.01	0.01	
		0.004665	0.0004767	0.002571	
MMS3_FM1513	2024_093/10:41:12 to 2024_093/10:41:42		0.0516	-0.1391	-0.2272	
		0.01	0.01	0.01	
		-0.0056	-0.0008692	0.004446	
MMS2_FM1513	2024_093/12:11:12 to 2024_093/12:12:22		0.0156	0.1109	-0.3089	
		0.01	0.01	0.01	
		-0.009963	0.0001083	0.003366