FR1120

Looking at the Restart states from Rev 1121 we have the following results for FR1120
FR1120		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	06/25/2020 07:57:35	97270.435	97263.657	97263.673	-6.777	-6.761	-0.01642	0.242%	5.671%
	
MMS2	06/25/2020 07:57:41	97263.672	97263.637	97263.656	-0.035	-0.016	-0.01851			
MMS3	06/25/2020 07:58:04	97255.706	97263.650	97263.610	7.944	7.904	0.04041	0.509%	-0.153%	
MMS4	06/25/2020 07:58:10	97258.920	97263.656	97263.682	4.737	4.762	-0.02545	-0.537%	3.192%	
 
MMS1 was 0.188 m/s (net delta-v) and 41.44% axial, MMS3 was 0.417 m/s and 30.79% axial, and MMS4 was 0.317 m/s and 39.39% 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 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)	
MMS3_FR1120	2020_173/02:59:07 to 2020_173/02:59:37		0.1057	-0.3881	0.0113	
		0.002	0.003881	0.002	
		0.0003495	-0.001529	-0.0007886	
MMS4_FR1120	2020_173/04:49:07 to 2020_173/04:49:37		0.1109	-0.2749	0.0671	
		0.002	0.002749	0.002	
		-0.0005112	-0.0006828	-0.0002541	
MMS1_FR1120	2020_173/06:39:17 to 2020_173/06:39:37		-0.1568	-0.025	0.1003	
		0.002	0.002	0.002	
		-0.0003762	-0.0005629	0.0002013