FM1387

Looking at the Restart states from Rev 1388 we have the following results for FM1387
FM1387		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 18 2023 13:17:24	97446.505	97439.603	97439.474	-6.903	-7.031	0.129	-1.862%	-0.122%	
MMS2	Jan 18 2023 13:16:53	97446.577	97428.673	97428.542	-17.904	-18.035	0.131	-0.731%	-1.154%	
MMS3	Jan 18 2023 13:16:32	97446.459	97426.238	97426.134	-20.220	-20.325	0.105	-0.519%	0.282%	
MMS4	Jan 18 2023 13:17:32	97446.568	97446.568	97446.590	0.000	0.022	-0.022			
 
MMS1 was 0.2356 m/s (net delta-v) and 1.55% axial, MMS2 was 0.2033 m/s and 15.07% axial, and MMS3 was 0.3527 m/s and 57.53% 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)	
MMS3_FM1387	2023_016/07:41:12 to 2023_016/07:42:12		0.0921	-0.0493	-0.3337	
		0.01	0.01	0.01	
		0.003232	-0.001953	0.002123	
MMS2_FM1387	2023_016/09:11:12 to 2023_016/09:11:32			0.1861	-0.0536	-0.0636	
		0.01	0.01	0.01	
		0.004544	-0.000247	0.0035	
MMS1_FM1387	2023_016/10:41:12 to 2023_016/10:41:32		-0.058	-0.2085	-0.0996	
		0.01	0.01	0.01	
		0.004469	0.007441	0.002966