FR1433

Looking at the Restart states from Rev 1434 we have the following results for FR1433
FR1433		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	Jun 28 2023 17:11:59	97388.458	97388.458	97388.443	0.000	-0.014	0.014			
MMS2	Jun 28 2023 17:12:10	97388.474	97399.476	97399.301	11.002	10.827	0.175	1.595%	-0.365%	
MMS3	Jun 28 2023 17:11:32	97388.518	97380.066	97379.784	-8.453	-8.734	0.282	-3.331%	-0.035%	
MMS4	Jun 28 2023 17:11:57	97388.525	97385.952	97385.863	-2.573	-2.662	0.089	-3.448%	-0.076%	
 
MMS2 was 0.2776 m/s (net delta-v) and 4.93% axial, MMS3 was 0.1705 m/s and 69.79% axial, and MMS4 was 0.2085 m/s and 51.60% 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 MMS2 DVZ and MMS3 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_FR1433	2023_177/11:36:12 to 2023_177/11:36:42			-0.2476	-0.1263	-0.0319	
		0.01	0.01	0.01	
		-0.003795	0.002321	0.01174	
MMS3_FR1433	2023_177/16:06:12 to 2023_177/16:06:52		0.0324	0.0867	-0.1449	
		0.01	0.01	0.01	
		-0.008473	0.000569	0.01199	
MMS4_FR1433	2023_177/17:41:12 to 2023_177/17:41:42		-0.0871	-0.0475	-0.1841	
		0.01	0.01	0.01	
		0.008582	-0.003345	0.004549