Table 3. Estimated LV target insertion performances (C3, RAV, and DAV), OD uncertainties and associated planned TCM-1 Delta-V magnitudes using tracking measurements of 8, 25, and 34 hours after launch

Variable		C3 (km2/s2)	RAV (deg)	DAV (deg)	OD uncertainty, 3-sigma, 3D RMS		Planned TCM-1 Delta-V mag. (m/s)
					Pos. (m)	Vel. (cm/s)
Target		−0.674	161.133	8.105	NA	NA	NA
Achieved (with OD sols.)	8 hour	−0.667	161.211	8.143	669.770	3.361	3.069
	25 hour	−0.667	161.212	8.147	386.424	0.948	3.080
	34 hour	−0.667	161.212	8.147	523.631	0.945	3.080
Delta (achieved – target)	8 hour	0.007	0.078	0.038	NA	NA	NA
	25 hour	0.007	0.079	0.042	NA	NA	NA
	34 hour	0.007	0.079	0.042	NA	NA	NA

LV, launch vehicle; C3, launch injection energy per unit mass; RAV, right ascension of the injection orbit apoapsis vector; DAV, declination of the injection orbit apoapsis vector; OD, orbit determination; RMS, root mean square; TCM, trajectory correction maneuver; NA, not applicable.