FR1259

Looking at the Restart states from Rev 1260 we have the following results for FR1259
FR1259		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 25 2021 10:03:44	97689.052	97704.097	97704.161	15.045	15.109	-0.064	-0.423%	-7.901%	
MMS2	Oct 25 2021 10:04:01	97689.490	97704.091	97704.175	14.601	14.685	-0.084	-0.573%	0.552%	
MMS3	Oct 25 2021 10:03:58	97704.169	97704.093	97704.132	-0.076	-0.037	-0.039			
MMS4	Oct 25 2021 10:03:44	97718.543	97704.124	97704.204	-14.419	-14.339	-0.080	0.556%	0.699%	
 
Note that MMS3 plane change was more than an order of magnitude small than that of MMS2.
MMS1 was 0.6546 m/s (net delta-v) and 22.77% axial, MMS2 was 0.7371 m/s and 37.90% axial, and MMS4 was 0.3299 m/s and 16.38% 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 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_FR1259	2021_294/00:29:07 to 2021_294/00:29:37		-0.2518	0.2145	0.0301	
		0.002518	0.002145	0.002	
		-0.0007123	0.0007436	0.004183	
MMS2_FR1259	2021_294/02:33:27 to 2021_294/02:34:37
	0.3493	-0.6415	0.0841	
		0.003493	0.006415	0.002	
		0.001439	-0.0037030	0.001175	
MMS1_FR1259	2021_294/04:23:37 to 2021_294/04:24:37		0.3481	-0.5483	-0.0726	
		0.003841	0.005483	0.002	
		0.002022	0.0009626	-0.001285