FR1052

Looking at the Restart states from Rev 1053 we have the following results for FR1052
FR1052		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	Oct 31 2019 06:25:48.813	97344.699	97341.904	97341.894	-2.795	-2.805	0.01043	-0.373%	
MMS2	Oct 31 2019 06:25:53.699	97344.693	97344.693	97344.700	0.000	0.007	-0.00674		
MMS3	Oct 31 2019 06:25:21.235	97344.656	97338.179	97338.231	-6.477	-6.425	-0.05222	0.806%	
MMS4	Oct 31 2019 06:24:58.541	97344.502	97336.912	97336.870	-7.590	-7.631	0.04149	-0.547%	
 
MMS1 was 0.091 m/s (net delta-v) and 24.39% axial, MMS3 was 0.38 m/s and 60.03% axial, and MMS4 was 0.17 m/s and 15.38% 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. 

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_FR1052	2019_301/18:46:12 to 2019_301/18:46:12*	0.0851	-0.0036	-0.0293	
		0.01	0.01	0.01	
		0.0007210	-0.0014800	-0.0002498	
MMS4_FR1052	2019_301/21:46:12 to 2019_301/21:46:22	-0.0133	-0.138	-0.0965	
		0.01	0.01	0.01	
		0.0003598	-0.0008283	-0.0015114	
MMS3_FR1052	2019_301/23:21:12 to 2019_301/23:22:22	0.1496	-0.0163	0.3478	
		0.01	0.01	0.01	
		0.0013120	-0.0012915	-0.0003972