FR1037

Looking at the Restart states from Rev 1038 we have the following results for FR1037
FR1037		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	Sep 08 2019 17:32:43.526	97446.494	97447.507	97447.601	1.014	1.107	-0.09303	-9.177%	
MMS2	Sep 08 2019 17:32:39.542	97446.630	97446.630	97446.667	0.000	0.036	-0.03641		
MMS3	Sep 08 2019 17:32:09.201	97446.615	97443.164	97443.209	-3.451	-3.407	-0.04446	1.288%	
MMS4	Sep 08 2019 17:32:06.806	97446.643	97444.615	97444.527	-2.028	-2.117	0.08863	-4.371%	
 
MMS1 was 0.15 m/s (net delta-v) and 44.47% axial, MMS3 was 0.11 m/s and 18.38% axial, and MMS4 was 0.12 m/s and 65.56% 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 

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)	
MMS1_FR1037	2019_249/07:16:12 to 2019_249/07:16:32	0.1018	0.0845	-0.0667	
		0.01	0.01	0.01	
		-0.001803	0.0009389	0.0001582	
MMS3_FR1037	2019_249/08:51:12 to 2019_249/08:51:22	0.1027	0.0114	-0.0168	
		0.01	0.01	0.01	
		-0.002348	0.001418	0.0003631	
MMS4_FR1037	2019_249/16:01:12 to 2019_249/16:01:32	0.0291	0.0203	-0.1165	
		0.01	0.01	0.01	
		-0.01048	0.005004	0.001892