FR1151

Looking at the Restart states from Rev 1152 we have the following results for FR1151
FR1151		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	10/11/2020 17:12:15	97447.071	97470.171	97470.259	23.101	23.188	-0.088	-0.379%	0.639%	
MMS2	10/11/2020 17:12:07	97445.116	97470.138	97470.198	25.022	25.082	-0.060	-0.242%	4.104%	
MMS3	10/11/2020 17:11:57	97470.285	97470.236	97470.252	-0.049	-0.033	-0.016			
MMS4	10/11/2020 17:12:10	97469.443	97470.244	97470.242	0.801	0.800	0.002	0.198%	0.885%	

MMS1 was 0.863 m/s (net delta-v) and 7.18% axial, MMS2 was 0.677 m/s and 30.81% axial, and MMS4 was 0.155 m/s and 40.41% 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 except MMS4 DVY, 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)	
MMS2_FR1151	2020_281/06:43:37 to 2020_281/06:44:37		0.278	-0.6185	0.0057	
		0.00278	0.006185	0.002	
		0.002702	0.004639	0.002501	
MMS4_FR1151	2020_281/12:04:17 to 2020_281/12:04:37		-0.0489	-0.0723	-0.1288	
		0.002	0.002	0.002	
		-0.0003036	-0.003265	-0.01488	
MMS1_FR1151	2020_281/16:48:17 to 2020_281/16:49:37		0.6156	-0.5458	-0.2686	
		0.006156	0.005458	0.002686	
		-0.004066	0.003846	0.001186