The initial velocity and apparent radiant were used to compute the orbit following procedures described by Ceplecha (1987). The orbit is presented in Table 5 and is of low eccentricity and low inclination with aphelion close to the Mars orbit.

**Table 5:** Radiant and orbit; angular elements referred to J2000
$\begin{tabular} {llr@{.}lcr@{.}l} \hline \multicolumn{7}{c}{}\\ $v_\infty$\spac... ...&0002 \\ $i$\space & degrees & 11&5 & $\pm$\space & 1&0 \\ \hline\end{tabular}$ $\begin{tabular} {lllll} \multicolumn{5}{l}{$v_\infty$\space initial velocity,}\\... ...lticolumn{5}{l}{standard notation for orbital elements is used.}\\ \end{tabular}$

7 Orbit