FR1119

Looking at the Restart states from Rev 1120 we have the following results for FR1119
FR1119		NoBurn	Plan	OD	Plan-NoBurn	OD-NoBurn	Plan-OD	SMA error	PC error	
MMS	Epoch of Plan Apogee	A(km)	A (km)	A (km)	A (km)	A (km)	A (km)			
MMS1	06/21/2020 20:05:35	97239.719	97246.481	97246.515	6.762	6.795	-0.03358	-0.497%	*	
MMS2	06/21/2020 20:05:27	97239.681	97239.681	97239.755	0.000	0.073	-0.07348			
MMS3	06/21/2020 20:05:12	97239.565	97231.841	97231.788	-7.724	-7.777	0.05290	-0.685%	0.644%	
MMS4	06/21/2020 20:05:28	97239.717	97234.957	97234.994	-4.760	-4.723	-0.03690	0.775%	0.057%	
 
MMS1 was 0.271 m/s (net delta-v) and 38.37% axial, MMS3 was 0.165 m/s and 57.34% axial, and MMS4 was 0.165 m/s and 3.26% axial.
The MMS1 plane change was two orders of magnitude smaller than the others.
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 meet the requirement except MMS1 DVX, MMS4 DVZ

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_FR1119	2020_171/10:41:12 to 2020_171/10:41:42		-0.2361	-0.0701	0.1289	
		0.01	0.01	0.01	
		0.01616	-0.001683	-0.00014	
MMS4_FR1119	2020_171/16:26:12 to 2020_171/16:26:22		-0.0754	-0.1454	-0.043	
		0.01	0.01	0.01	
		-2.48E-05	0.007504	0.01065	
MMS3_FR1119	2020_171/18:01:12 to 2020_171/18:01:42		0.0931	-0.041	0.1323	
		0.01	0.01	0.01	
		-0.005821	0.001491	-0.002431