Stereo-Vision-Based Relative Pose Estimation for the Rendezvous and Docking of Noncooperative Satellites

Table 1

Initial orbit elements.

	(km)		(°)	(°)	(°)	(°)
Target	6700	0	0	0	0	0
Chaser	6700	0	0	0	0	−8.5 × 10^−5