FM1187

Looking at the Restart states from Rev 1188 we have the following results for FM1187
FM1187		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	Feb 14 2021 21:35:28	97433.501	97433.725	97433.796	0.224	0.296	-0.072	-32.017%	0.540%	
MMS2	Feb 14 2021 21:35:22	97433.782	97433.725	97433.750	-0.057	-0.031	-0.025			
MMS3	Feb 14 2021 21:35:37	97427.078	97433.723	97433.769	6.645	6.692	-0.046	-0.694%	0.130%	
MMS4	Feb 14 2021 21:35:42	97425.025	97433.725	97433.813	8.700	8.788	-0.088	-1.008%	-1.072%	
 
MMS1 was 0.229 m/s (net delta-v) and 6.49% axial, MMS3 was 0.428 m/s and 30.21% axial, and MMS4 was 0.262 m/s and 39.91% 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, DVZ

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_FM1187	2021_41/15:24:70 to 2021_41/15:24:37		0.1895	0.1562	-0.0886	
		0.002	0.002	0.002	
		0.002215	0.004768	0.002766	
MMS1_FM1187	2021_41/23:44:17 to 2021_41/23:44:37		0.0024	0.2089	0.0832	
		0.002	0.002089	0.002	
		-0.003277	-0.001656	0.001745	
MMS3_FM1187	2021_42/01:33:57 to 2021_42/01:34:37		0.4022	-0.0949	0.1009	
		0.004022	0.002	0.002	
		0.004861	-0.002568	-0.0007753