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Table 2:

Orbital parameters.
Orbit id $r_{\rm ini}$ $v_{\rm ini}$ La Eb
  [kpc] [100 $\rm km~s^{-1}$] [ $10^2~\rm km~s^{-1}~kpc$] [ $10^4~ \rm km^2~s^{-2}$]
01 100. 2.0 57.0 0.
02 100. 3.0 59.0. 2.5
05 100. 2.0 80.0 0.
13 100. 0.0 0.0 -2.
14 70.0 1.5 41.3 -0.66
15 70.0 1.6 41.3 -1.57
a It is the absolute value of the angular momentum of the unit mass, i.e., $L=\mid
\vec{r} \times \vec{v}\mid $. b It is the total energy of the relative motion, i.e., E=v2/2-G(m1+m2)/r, with $m_1=m_2=2.3 \times10^{11}~M_{\odot}$.

Source LaTeX | All tables | In the text

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