FR1038

Looking at the Restart states from Rev 1039 we have the following results for FR1038
FR1038		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 12 2019 05:42:28.252	97488.367	97487.500	97487.539	-0.866	-0.827	-0.03904	4.506%	
MMS2	Sep 12 2019 05:42:29.917	97487.496	97487.496	97487.527	0.000	0.030	-0.03042		
MMS3	Sep 12 2019 05:42:15.703	97484.009	97487.487	97487.469	3.478	3.460	0.01797	0.517%	
MMS4	Sep 12 2019 05:42:07.717	97485.423	97487.445	97487.311	2.023	1.888	0.13436	6.643%	
 
MMS1 was 0.071 m/s (net delta-v) and 1.43% axial, MMS3 was 0.16 m/s and 21.69% axial, and MMS4 was 0.11 m/s and 10.74% 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_FR1038	2019_251/5:59:37 to 2019_251/5:59:37*	-0.0152	0.0623	0.0268	
		0.002	0.002	0.002	
		-0.0008881	0.0007088	0.0005397	
MMS3_FR1038	2019_251/7:49:27 to 2019_251/7:49:37	0.1277	-0.0933	0.0098	
		0.002	0.002	0.002	
		-0.0008632	0.0007713	0.0001505	
MMS4_FR1038	2019_251/14:59:27 to 2019_251/14:59:37	0.1305	-0.0268	0.0103	
		0.002	0.002	0.002	
		-0.001109	0.0009055	0.0002869