FR1222

Looking at the Restart states from Rev 1223 we have the following results for FR1222
FR1222		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	Jun 17 2021 13:03:43	97442.226	97447.511	97447.524	5.285	5.298	-0.013	-0.250%	1.224%	
MMS2	Jun 17 2021 13:03:44	97442.209	97442.209	97442.280	0.000	0.071	-0.071			
MMS3	Jun 17 2021 13:03:50	97442.227	97438.092	97438.085	-4.135	-4.142	0.006	-0.152%	0.278%	
MMS4	Jun 17 2021 13:03:54	97442.253	97438.530	97438.562	-3.723	-3.691	-0.032	0.850%	0.352%	
 
MMS1 was 0.479 m/s (net delta-v) and 44.25% axial, MMS3 was 0.231 m/s and 71.25% axial, and MMS4 was 0.269 m/s and 9.26% 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)	
MMS3_FR1222	2021_165/15:16:12 to 2021_165/15:17:02		0.065	-0.0737	0.2025	
		0.01	0.01	0.01	
		0.003212	0.0007481	0.001585	
MMS1_FR1222	2021_165/16:51:12 to 2021_165/16:52:12	-0.3697	-0.0364	0.2981	
		0.01	0.01	0.01	
		0.0004812	-2.44E-05	0.0001154	
MMS4_FR1222	2021_165/18:26:12 to 2021_165/18:26:32		-0.1751	-0.1835	-0.0884	
		0.01	0.01	0.01	
		0.001143	0.0002458	0.0004437