FR1706

Looking at the Restart states from Rev 1707 we have the following results for FR1706
FR1706		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	Feb 12 2026 11:28:38	97860.163	97860.163	97860.240	0.000	0.078	-0.078	 		
MMS2	Feb 12 2026 11:29:06	97860.168	97858.260	97858.368	-1.908	-1.800	-0.108	5.648%	0.304%	
MMS3	Feb 12 2026 11:29:10	97860.159	97856.937	97857.053	-3.223	-3.107	-0.116	3.588%	-5.919%	
MMS4	Feb 12 2026 11:28:13	97860.157	97846.884	97846.893	-13.273	-13.264	-0.009	0.068%	1.410%	
 
MMS2 was 0.4462 m/s (net delta-v) and 66.99% axial, MMS3 was 0.3380 m/s and 46.81% axial, and MMS4 was 0.2324 m/s and 26.68% axial.
Larger % errors on MMS2 due to maneuver being much smaller than the other two. 

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.
Mnvr ID	Time Span	DeltaV_X (m/s)	DeltaV_X Req (m/s)	Diff_V_X (m/s)	DeltaV_Y (m/s)	DeltaV_Y Req (m/s)	Diff_V_Y (m/s)	DeltaV_Z (m/s)	DeltaV_Z Req (m/s)	Diff_V_Z (m/s)	
MMS4	2026_41/01:01:12 to 2026_41/01:01:32	0.182	0.01	-0.0005367	-0.1434	0.01	0.002031	0.0044	0.01	0.0003881	
MMS3	2026_41/02:26:12 to 2026_41/02:27:02	0.2012	0.01	0.000167	0.0737	0.01	0.0004154	0.2614	0.01	-0.0005655	
MMS2	2026_41/03:46:12 to 2026_41/03:47:42	0.0349	0.01	0.001705	-0.3447	0.01	-0.0002138	0.2805	0.01	0.0001861