FR1150

Looking at the Restart states from Rev 1151 we have the following results for FR1150
FR1150		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	10/08/2020 05:03:41	97435.495	97412.304	97412.320	-23.191	-23.175	-0.016	0.068%	0.337%	
MMS2	10/08/2020 05:03:46	97435.723	97410.395	97410.358	-25.327	-25.364	0.037	-0.147%	0.359%	
MMS3	10/08/2020 05:04:56	97435.423	97435.423	97435.489	0.000	0.066	-0.066			
MMS4	10/08/2020 05:05:05	97435.543	97434.581	97434.643	-0.962	-0.900	-0.063	6.500%	0.218%	
 
MMS1 was 0.469 m/s (net delta-v) and 12.88% axial, MMS2 was 0.352 m/s and 22.88% axial, and MMS4 was 0.337 m/s and 70.99% 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 DVX, 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)	
MMS4_FR1150	2020_279/15:26:12 to 2020_279/15:27:22		0.0166	-0.0301	0.3349	
		0.01	0.01	0.01	
		-0.105	0.002348	-0.0493	
MMS1_FR1150	2020_279/20:26:12 to 2020_279/20:26:52		0.4631	-0.0288	0.0794	
		0.01	0.01	0.01	
		0.009204	0.0001651	-0.001512	
MMS2_FR1150	2020_279/22:01:12 to 2020_279/22:01:42		0.3114	-0.1589	0.0454	
		0.01	0.01	0.01	
		0.003053	-0.001017	0.0005863