FR1367

Looking at the Restart states from Rev 1368 we have the following results for FR1367
FR1367		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	Nov 09 2022 10:32:53	97414.446	97400.170	97400.106	-14.277	-14.340	0.063	-0.445%	2.204%	
MMS2	Nov 09 2022 10:32:37	97408.968	97400.122	97400.204	-8.846	-8.764	-0.082	0.922%	-5.428%	
MMS3	Nov 09 2022 10:32:31	97400.160	97400.109	97400.126	-0.051	-0.034	-0.017	 		
MMS4	Nov 09 2022 10:32:38	97406.730	97400.139	97400.177	-6.591	-6.553	-0.038	0.584%	0.595%	
 
MMS1 was 0.4828 m/s (net delta-v) and 15.75% axial, MMS3 was 0.7433 m/s and 5.72% axial, and MMS4 was 0.1760 m/s and 7.03% axial.
The small axial percentages explain the large percentage PC errors.
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 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)	
MMS4_FR1367	2022_309/01:24:27 to 2022_309/01:24:37	-0.091	0.0891	-0.0072	
		0.002	0.002	0.002	
		0.004035	-0.002550	-0.005462	
MMS1_FR1367	2022_309/07:33:47 to 2022_309/07:34:37	-0.3747	0.3287	0.1701	
		0.003747	0.003287	0.002	
		-0.009800	0.007118	0.004167	
MMS2_FR1367	2022_309/09:23:47 to 2022_309/09:24:37			-0.3306	0.3879	0.1077	
		0.003306	0.003879	0.002	
		-0.002425	0.002696	0.003846