FR1707

Looking at the Restart states from Rev 1709 we have the following results for FR1707
FR1707		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 19 2026 13:02:06	98028.308	98028.253	98028.268						
MMS2	Feb 19 2026 13:02:21	98026.469	98028.274	98028.281	1.805	1.812	-0.007	-0.413%	0.085%	
MMS3	Feb 19 2026 13:02:11	98025.158	98028.254	98028.357	3.096	3.199	-0.103	-3.329%	25.113%	
MMS4	Feb 19 2026 13:02:19	98015.031	98028.306	98028.377	13.275	13.347	-0.072	-0.539%	-1.349%	
 
MMS2 was 0.2852 m/s (net delta-v) and 30.75% axial, MMS3 was 0.2898 m/s and 23.19% axial, and MMS4 was 0.78173 m/s and 36.58% axial.
Large PC errors on MMS3 due to very small plane change (by a factor of over 100) for MMS3.  

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)	
MMS2	2026_43/12:24:17 to 2026_43/12:24:37	-0.0801	0.002	0.0004724	0.2711	0.002711	7.804e-05	0.0144	0.002	0.001871	
MMS3	2026_43/13:59:07 to 2026_43/13:59:37	-0.2447	0.002447	0.000167	0.0819	0.002	0.001274	0.1311	0.002	-0.0001653	
MMS4	2026_43/15:33:27 to 2026_43/15:34:37	0.6437	0.006437	0.001594	0.1551	0.002	0.000784	0.416	0.00416	-0.0007217