FR1366

Looking at the Restart states from Rev 1367 we have the following results for FR1366
FR1366		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 05 2022 22:32	97411.577	97425.533	97425.623	13.956	14.046	-0.090	-0.646%	1.169%	
MMS2	Nov 05 2022 22:32:05	97411.673	97420.098	97420.133	8.425	8.460	-0.035	-0.415%	1.515%	
MMS3	Nov 05 2022 22:30:54	97411.327	97411.327	97411.343	0.000	0.016	-0.016			
MMS4	Nov 05 2022 22:31:16	97411.389	97417.865	97417.919	6.476	6.530	-0.054	-0.837%	0.161%	
 
MMS1 was 0.4530 m/s (net delta-v) and 55.4% axial, MMS3 was 0.1696 m/s and 70.88% axial, and MMS4 was 0.3654 m/s and 83.40% 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 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)	
MMS1_FR1366	2022_307/11:51:12 to 2022_307/11:52:12		-0.2279	-0.109	0.2383	
		0.01	0.01	0.01	
		0.005346	-0.002758	-0.007588	
MMS4_FR1366	2022_307/13:26:12 to 2022_307/13:26:52			0.0105	-0.0296	0.1947	
		0.01	0.01	0.01	
		-0.010590	-0.004972	0.007592	
MMS2_FR1366	2022_307/15:01:12 to 2022_307/15:01:32		-0.0683	-0.0057	0.1086	
		0.01	0.01	0.01	
		-0.004075	0.002051	0.001694