FM1305

Looking at the Restart states from Rev 1305 we have the following results for FM1305
FM1305		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 05 2022 08:48:06	97676.247	97671.430	97671.353	-4.817	-4.894	0.077	-1.599%	2.679%	
MMS2	Apr 05 2022 08:48:03	97683.454	97671.305	97671.311	-12.149	-12.143	-0.006	0.052%	0.196%	
MMS3	Apr 05 2022 08:47:57	97681.161	97671.261	97671.307	-9.900	-9.854	-0.047	0.471%	1.415%	
MMS4	Apr 05 2022 08:48:19	97671.435	97671.327	97671.339	-0.108	-0.096	-0.011			
 
MMS1 was 0.3179 m/s (net delta-v) and 44.42% axial, MMS2 was 0.5542 m/s and 3.35% axial, and MMS3 was 0.5541 m/s and 5.74% 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, almost all are slightly higher than the requirement.  Only MMS3 DVY and MMS2 DVY 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_FM1305	2022_91/00:13:57 to 2022_91/00:14:37	-0.1521	0.2623	-0.091	
		0.002	0.002623	0.002	
		-0.006381	0.009816	0.009370	
MMS3_FM1305	2022_91/07:43:47 to 2022_91/07:44:37
	-0.3205	0.3985	0.2103	
		0.003205	0.003985	0.002103	
		-0.004674	0.003471	0.003967	
MMS2_FM1305	2022_91/09:33:47 to 2022_91/09:34:37
	-0.489	0.2363	0.1095	
		0.00489	0.002363	0.002	
		-0.004932	0.001676	0.002025