FM1024

Looking at the Restart states from Rev 1025 we have the following results for FM1024
FM1024		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 25 2019 04:10:38.412	97378.227	97379.153	97379.172	0.926	0.945	-0.01892	-2.043%	
MMS2	Jul 25 2019 04:10:30.151	97378.126	97378.126	97378.119	0.000	-0.007	0.00690		
MMS3	Jul 25 2019 04:10:09.885	97378.203	97379.246	97379.287	1.043	1.084	-0.04144	-3.975%	
MMS4	Jul 25 2019 04:09:52.575	97378.120	97376.073	97376.066	-2.047	-2.054	0.00677	-0.331%	
 
MMS1 was 0.0073 m/s (net delta-v) and 53.01% axial, MMS3 was 0.0058 m/s and 38.07% axial, and MMS4 was 0.0057 m/s and 48.86% 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 MMS4 DVX, MMS4 DVY, MMS1 DVX, and MMS1 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_FM1024	2019_203/20:21:12 to 2019_203/20:21:22	-0.0476	-0.0264	0.0393	
		0.01	0.01	0.01	
		-0.008146	0.007626	0.001522	
MMS4_FM1024	2019_204/01:11:12 to 2019_204/01:11:22	0.0366	-0.0059	-0.0434	
		0.01	0.01	0.01	
		-0.02502	0.01456	0.003861	
MMS1_FM1024	2019_204/02:36:12 to 2019_204/02:36:22	0.0269	0.0399	-0.0421	
		0.01	0.01	0.01	
		-0.03108	0.01562	0.004963