FM1304

Looking at the Restart states from Rev 1305 we have the following results for FM1304
FM1304		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 01 2022 20:25:50	97665.247	97670.130	97670.182	4.883	4.934	-0.052	-1.058%	0.463%	
MMS2	Apr 01 2022 20:26:22	97665.350	97677.346	97677.391	11.996	12.040	-0.044	-0.370%	0.767%	
MMS3	Apr 01 2022 20:26:15	97665.338	97675.110	97675.100	9.772	9.763	0.010	0.099%	-0.191%	
MMS4	Apr 01 2022 20:25:41	97665.336	97665.336	97665.399	0.000	0.063	-0.063			
 
MMS1 was 0.2824 m/s (net delta-v) and 26.65% axial, MMS2 was 0.2853 m/s and 35.76% axial, and MMS3 was 0.2883 m/s and 59.89% 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 MMS2 DVY and DVZ. 

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)	
MMS2_FM1304	2022_89/04:21:12 to 2022_89/04:21:42		-0.1441	0.1329	0.2056	
		0.01	0.01	0.01	
		-0.008390	0.012760	0.015230	
MMS1_FM1304	2022_89/05:56:12 to 2022_89/05:56:32		0.1344	0.2455	0.0036	
		0.01	0.01	0.01	
		0.002226	-0.007818	-0.002584	
MMS3_FM1304	2022_89/11:21:12 to 2022_89/11:22:02		-0.1549	0.1484	-0.193	
		0.01	0.01	0.01	
		0.003914	-0.007173	0.004412