FM1025

Looking at the Restart states from Rev 1026 we have the following results for FM1025
FM1025		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)		
MMS1	Jul 28 2019 16:13:52.056	97422.677	97421.638	97421.613	-1.039	-1.064	0.02499	-2.406%	
MMS2	Jul 28 2019 16:13:51.106	97421.630	97421.617	97421.617	-0.014	-0.014	0.00015		
MMS3	Jul 28 2019 16:13:29.071	97422.795	97421.777	97421.574	-1.018	-1.221	0.20289	-19.928%	
MMS4	Jul 28 2019 16:13:20.867	97419.570	97421.623	97421.698	2.054	2.129	-0.07526	-3.665%	
 
MMS1 was 0.117 m/s (net delta-v) and 37.91% axial, MMS3 was 0.0075 m/s and 45.90% axial, and MMS4 was 0.111 m/s and 59.33% 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 maneuvering spacecraft meet the requirement, except MMS3 DVY 

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_FM1025	2019_205/00:54:27 to 2019_205/00:54:37	0.0027	0.004	0.0671	
		0.002	0.002	0.002	
		0.0001507	0.002047	-0.0002237	
MMS4_FM1025	2019_205/02:59:17 to 2019_205/02:59:37	-0.0028	-0.1064	0.0703	
		0.002	0.002	0.002	
		-0.0001649	0.001919	-0.000318	
MMS1_FM1025	2019_205/22:14:27 to 2019_205/22:14:37	-0.02	0.0509	0.0826	
		0.002	0.002	0.002	
		-0.001067	0.001948	0.000299