Low-Thrust Trajectory Design Using Finite Fourier Series Approximation of Pseudoequinoctial Elements

Table 1

Classical orbital elements of 1989ML and Temple-1 at the given epoch MJD.

Parameter	(DU)		(°)	(°)	(°)	(°)	Epoch (MJD)
1989ML	1.2721	0.13649	4.3782	104.3571	183.3249	117.36689	53900
Tempel-1	3.14009	0.51159	10.5052	68.8818	179.3031	203.23760	56717