FR1493

Looking at the Restart states from Rev 1494 we have the following results for FR1493
FR1493		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	Jan 25 2024 05:37:09	97758.390	97757.892	97757.893	-0.498	-0.497	-0.001	0.219%	1.094%	
MMS2	Jan 25 2024 05:36:48	97758.090	97757.233	97757.239	-0.857	-0.852	-0.006	0.689%	0.398%	
MMS3	Jan 25 2024 05:37:04	97758.335	97758.335	97758.411	0.000	0.076	-0.077			
MMS4	Jan 25 2024 05:36:25	97758.358	97753.873	97753.786	-4.485	-4.572	0.087	-1.929%	0.204%	
 
MMS1 was 0.12561 m/s (net delta-v) and 25.31% axial, MMS2 was 0.23337 m/s and 32.66% axial, and MMS4 was 0.14937 m/s and 61.47% 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.

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_FR1493	2024_22/20:25:15 to 2024_22/20:26:42		0.0832	0.0602	0.0726	
		0.01	0.01	0.01	
		-0.003648	-0.001305	-0.003899	
MMS2_FR1493	2024_22/22:00:13 to 2024_22/22:01:56		0.0924	0.2119	-0.0062	
		0.01	0.01	0.01	
		0.003838	-0.0003495	-0.00233	
MMS4_FR1493	2024_23/01:10:21 to 2024_23/01:11:58		0.0395	0.1082	-0.0935	
		0.01	0.01	0.01	
		0.005764	-0.0005435	-0.002638