FR1348

Looking at the Restart states from Rev 1349 we have the following results for FR1348
FR1348		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	Sep 03 2022 16:49:13	97710.971	97720.104	97720.138	9.133	9.166	-0.033	-0.365%	0.878%	
MMS2	Sep 03 2022 16:49:06	97720.120	97720.099	97720.105	-0.021	-0.015	-0.006			
MMS3	Sep 03 2022 16:48:37	97727.014	97720.097	97720.061	-6.917	-6.954	0.036	-0.526%	0.193%	
MMS4	Sep 03 2022 16:48:42	97731.860	97720.089	97720.090	-11.771	-11.770	-0.001	0.006%	0.447%	
 
MMS1 was 0.2186 m/s (net delta-v) and 32.98% axial, MMS3 was 0.3251 m/s and 10.56% axial, and MMS4 was 0.6614 m/s and 26.57% 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, most of them just barely do not 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)	
MMS1_FR1348	2022_242/9:29:17 to 2022_242/9:29:37			0.1911	0.0822	-0.0592	
		0.002	0.002	0.002	
		0.003525	-0.002583	-0.004330	
MMS3_FR1348	2022_242/15:29:07 to 2022_242/15:29:37		-0.2885	0.1496	0.0132	
		0.002885	0.002	0.002	
		-0.003344	0.004478	-0.003254	
MMS4_FR1348	2022_242/17:28:37 to 2022_242/17:29:37		-0.4231	0.3702	0.3473	
		0.004231	0.003702	0.003473	
		-0.004528	0.003224	0.002079