Prediction of Orbit Decay for Large-Scale Spacecraft considering Rarefied Aerodynamic Perturbation Effects

Table 2

Parameters in computing the TLE data with drag term.

Variables
	0.0011	0.0019
	42.7415	42.7440
	208.7171	208.7117
	346.3459	349.7146
	37.7664	36.4448
	0.0713	0.0711