FR1100

Looking at the Restart states from Rev 1101 we have the following results for FR1100
FR1100		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	04/16/2020 10:41:59	97520.354	97524.809	97524.907	4.455	4.553	-0.09736	-2.185%	-1.801%	
MMS2	04/16/2020 10:41:53	97520.395	97520.395	97520.495	0.000	0.100	-0.10018			
MMS3	04/16/2020 10:42:04	97520.419	97520.321	97520.447	-0.097	0.028	-0.12579	129.050%	1.605%	
MMS4	04/16/2020 10:42:10	97520.431	97521.135	97521.215	0.704	0.784	-0.07977	-11.324%	-1.460%	
 
MMS1 was 0.181 m/s (net delta-v) and 27.23% axial, MMS3 was 0.128 m/s and 67.74% axial, and MMS4 was 0.162 m/s and 1.56% axial.
The MMS3 SMA change was so small compared to OD error that is was not an observable.  The plane change is a more valid indicator.

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 maneuvering spacecraft 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_FR1100	2020_104/23:16:12 to 2020_104/23:16:22 	-0.1681	-0.0311	0.0644	
		0.01	0.01	0.01	
		0.00442	0.002036	0.003735	
MMS3_FR1100	2020_105/0:51:12 to 2020_105/0:51:42 	-0.031	-0.0367	0.1217	
		0.01	0.01	0.01	
		-0.004286	0.007796	0.006483	
MMS4_FR1100	2020_105/0:51:12 to 2020_105/0:51:42 	-0.1254	-0.0981	-0.036	
		0.01	0.01	0.01	
		-0.001328	0.003715	0.004985