FM1186

Looking at the Restart states from Rev 1187 we have the following results for FM1186
FM1186		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 11 2021 09:17:59	97609.148	97608.814	97608.830	-0.334	-0.318	-0.016	4.881%	0.060%	
MMS2	Feb 11 2021 09:17:40	97609.081	97609.081	97609.132	0.000	0.051	-0.050			
MMS3	Feb 11 2021 09:17:20	97609.111	97602.328	97602.336	-6.783	-6.775	-0.008	0.116%	0.297%	
MMS4	Feb 11 2021 09:17:46	97609.204	97600.339	97600.265	-8.865	-8.939	0.074	-0.837%	1.272%	
 
MMS1 was 0.384 m/s (net delta-v) and 49.62% axial, MMS3 was 0.326 m/s and 22.45% axial, and MMS4 was 0.272 m/s and 41.65% 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_FM1186	2021_39/11:36:12 to 2021_39/11:36:42		-0.0984	-0.2343	-0.1987	
		0.01	0.01	0.01	
		-0.001216	0.001851	0.005189	
MMS4_FM1186	2021_39/19:36:12 to 2021_39/19:36:42		0.2014	-0.0222	-0.1785	
		0.01	0.01	0.01	
		-0.006397	0.006768	0.005195	
MMS1_FM1186	2021_40/05:1:12 to 2021_40/05:2:12		-0.1728	-0.0909	-0.3219	
		0.01	0.01	0.01	
		0.00347	-0.001192	-0.002626