Table 5: Results for 67P/Churyumov-Gerasimenko.
Epoch 2003 Dec. 27.0 TT

Model 1 Model 2 Krolikowska (2003)

T 2002 Aug. 18.28687 Aug. 18.28715 Aug. 18.28695

$\omega$ 11.40963 11.40974 11.40976

$\Omega$ 50.92877 50.92869 50.92865

I 7.12417 7.12415 7.12415

q 1.2906480 1.2906474 1.2906479

e 0.6317508 0.6317510 0.6317509

A₁ +0.05089 $\pm 0.00271$ +0.06120 $\pm 0.00281$ +0.05444 $\pm 0.00267$

A₂ +0.00979 $\pm 0.00002$ +0.00991 $\pm 0.00001$ +0.00981 $\pm 0.00002$

A₃ +0.03552 $\pm 0.00214$ +0.02961 $\pm 0.00187$ +0.03386 $\pm 0.00215$

rms 1''57 1''57 1''16

**Table 5:** Results for 67P/Churyumov-Gerasimenko.
Epoch	2003 Dec. 27.0 TT
	Model 1	Model 2	Krolikowska (2003)
T	2002 Aug. 18.28687	Aug. 18.28715	Aug. 18.28695
$\omega$	11.40963	11.40974	11.40976
$\Omega$	50.92877	50.92869	50.92865
I	7.12417	7.12415	7.12415
q	1.2906480	1.2906474	1.2906479
e	0.6317508	0.6317510	0.6317509
A₁	+0.05089 $\pm 0.00271$	+0.06120 $\pm 0.00281$	+0.05444 $\pm 0.00267$
A₂	+0.00979 $\pm 0.00002$	+0.00991 $\pm 0.00001$	+0.00981 $\pm 0.00002$
A₃	+0.03552 $\pm 0.00214$	+0.02961 $\pm 0.00187$	+0.03386 $\pm 0.00215$
rms	1''57	1''57	1''16

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