FR1494

Looking at the Restart states from Rev 1495 we have the following results for FR1494
FR1494		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	Jan 28 2024 18:10:01	97772.096	97772.539	97772.641	0.444	0.546	-0.102	-23.01%	-0.570%	
MMS2	Jan 28 2024 18:09:49	97771.447	97772.542	97772.723	1.095	1.122	-0.027	-2.422%	0.612%	
MMS3	Jan 28 2024 18:09:59	97772.619	97772.542	97772.650	-0.077	0.031	-0.108	 		
MMS4	Jan 28 2024 18:09:43	97767.995	97772.582	97772.636	4.587	4.641	-0.054	-1.181%	-0.395%	
 
MMS1 was 0.12421 m/s (net delta-v) and 41.12% axial, MMS2 was 0.084627 m/s and 13.87% axial, and MMS4 was 0.220038 m/s and 13.63% axial.
MMS1 was highly axial so the place change error is more reflective of the maneuver error.
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, except MMS4 DVX.

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)	
MMS2_FR1494	2024_24/13:43:37 to 2024_24/13:44:59		0.0397	-0.0725	-0.0198	
		0.002	0.002	0.002	
		-0.001997	0.0008625	-0.0003729	
MMS1_FR1494	2024_24/15:58:27 to 2024_24/15:59:57		-0.0211	0.118	-0.0181	
		0.002	0.002	0.002	
		-0.000254	0.0003198		0.0004484	
MMS4_FR1494	2024_24/20:18:16 to 2024_24/20:20:03		0.2072	-0.0447	-0.0609	
		0.002072	0.002	0.002	
		0.002247	-0.001731		0.001521