FM1514

Looking at the Restart states from Rev 1515 we have the following results for FM1514
FM1514		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	Apr 08 2024 06:13:07	97773.425	97773.415	97773.392	-0.010	-0.033	0.023	 		
MMS2	Apr 08 2024 06:13:11	97762.617	97773.297	97773.379	10.680	10.762	-0.083	-0.774%	0.381%	
MMS3	Apr 08 2024 06:13:23	97758.640	97773.351	97773.450	14.711	14.810	-0.099	-0.676%	-0.124%	
MMS4	Apr 08 2024 06:13:24	97748.003	97773.404	97773.443	25.400	25.440	-0.040	-0.157%	1.770%	
 
MMS2 was 0.3823 m/s (net delta-v) and 16.29% axial, MMS3 was 0.60862 m/s and 19.28% axial, and MMS4 was 0.76026 m/s and 25.28% 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 MMS3 DVZ, MMS2 DVZ, MMS4 DVY

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)	
MMS3_FM1514	2024_094/20:03:37 to 2024_094/20:04:37		0.2425	-0.4521	-0.3242	
		0.002425	0.004521	0.003242	
		0.00143	-0.001596	-0.0005371	
MMS2_FM1514	2024_094/21:53:57 to 2024_094/21:54:37		0.2532	-0.2796	-0.0584	
		0.002532	0.002796	0.002	
		0.001885	0.002038	0.002839	
MMS4_FM1514	2024_094/23:43:27 to 2024_094/23:44:37		0.6115	-0.2781	-0.3663	
		0.006115	0.002781	0.003663	
		0.005068	0.00437	0.003095