Space-Based Optical Observations on Space Debris via Multipoint of View

Table 1

Initial conditions of parameters in the simulation.

(1) Initial condition of the orbit determination process	Initial state error
	Process noise matrix
	Filter	Extended information filter (EIF)
(2) Initial condition of the optical sensor	Measurement period	1 s
	Measurement error	5 arcsec
	FWHM	10 deg
	Maximal detectable magnitude ()	18
(3) Initial condition of the targets	Albedo ()	0.3
	Cross-sectional area ()	100 cm^2