AR1356

Looking at the Restart states from Rev 1358 we have the following results for AR1356
AR1356		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	Oct 05 2022 09:17:09	97874.195	97605.090	97604.849	-269.105	-269.346	0.24081	-0.089%	1.150%	
MMS2	Oct 05 2022 09:16:60	97874.149	97605.086	97605.004	-269.062	-269.144	0.08216	-0.031%	1.470%	
MMS3	Oct 05 2022 09:16:27	97874.152	97605.145	97604.702	-269.007	-269.450	0.44228	-0.164%	2.901%	
MMS4	Oct 05 2022 09:16:36	97874.174	97605.106	97604.727	-269.068	-269.447	0.37880	-0.141%	1.367%	
 
MMS1 was 0.86485 m/s (net delta-v) and 0.40% axial, MMS2 was 0.862427 m/s and 0.50% axial, MMS3 was 0.864499 m/s and 0.55% axial, and MMS4 was 0.865593 m/s and 0.53% 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 do not meet the requirement, as usual for apogee adjustments.

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_AR1356	2022_273/02:58:30 to 2022_273/02:59:50
	0.285	0.7438	0.3355	
		0.01	0.01	0.01	
		0.03439	0.09435	0.06805	
MMS2_AR1356	2022_273/02:58:20 to 2022_273/02:59:40
	0.2835	0.7425	0.3317	
		0.01	0.01	0.01	
		-0.09981	0.06733	0.05473	
MMS3_AR1356	2022_273/02:57:40 to 2022_273/02:59:00			0.288	0.7432	0.3359	
		0.01	0.01	0.01	
		0.06318	-0.09292	-0.02116	
MMS4_AR1356	2022_273/02:57:50 to 2022_273/02:59:10		0.2879	0.7432	0.3351	
		0.01	0.01	0.01	
		-0.155	0.1453	0.08129