Table 1: Orbit of Caliban from 47 obs. 1984-1998.
Epoch 1999 Jan. 22.0 TT

Model 1 Model 2

T 1998 Apr. 18.729 Apr. 18.709

$\omega$ 338.792 338.780

$\Omega$ 175.070 175.071

I 139.697 139.697

q 0.0439947 0.0439950

e 0.0814373 0.0814311

rms 0''63 0''63

**Table 1:** Orbit of Caliban from 47 obs. 1984-1998.
Epoch	1999 Jan. 22.0 TT
	Model 1	Model 2
T	1998 Apr. 18.729	Apr. 18.709
$\omega$	338.792	338.780
$\Omega$	175.070	175.071
I	139.697	139.697
q	0.0439947	0.0439950
e	0.0814373	0.0814311
rms	0''63	0''63

Source LaTeX | All tables | In the text

	1 Introduction
	2 Orbit model
	3 Applications to satellites and comets
	4 Conclusions
	References
	Online Material
	Appendix: Two-body partials