FM1626

Looking at the Restart states from Rev 1627 we have the following results for FM1626
FM1626		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	May 06 2025 23:06:04	97591.646	97597.840	97597.945	6.195	6.299	-0.104	-1.681%	-0.319%	
MMS2	May 06 2025 23:06:14	97591.905	97591.165	97591.121	-0.740	-0.784	0.044	-5.933%	0.374%	
MMS3	May 06 2025 23:06:23	97591.817	97596.336	97596.446	4.519	4.629	-0.110	-2.429%	0.251%	
MMS4	May 07 2025 01:02:10			97461.370				 		
 
MMS1 was 0.25062 m/s (net delta-v) and 20.54% axial, MMS2 was 0.41966 m/s and 56.62% axial, and MMS3 was 0.53112 m/s and 34.62% axial.
Larger % errors on MMS2 due to maneuver being much smaller than the other two.  There are some significant OD errors which most likely affect the results.

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.

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_FM1626	2025_124/16:01:12 to 2025_124/16:01:32		0.402	0.2028	0.1384	
		0.01	0.01	0.01	
		-0.001329	0.0008364	-0.003921	
MMS2_FM1626	2025_124/17:36:12 to 2025_124/17:37:22		0.0188	0.3567	-0.2152	
		0.01	0.01	0.01	
		-0.007409	-0.003029	0.001524	
MMS3_FM1626	2025_124/19:11:12 to 2025_124/19:12:20		0.0656	0.5219	-0.0392	
		0.01	0.01	0.01	
		-0.007274	0.0003322	-0.0003477