Table 3
Locations of hypothetical satellites that may hold an edge of a Chariklo ring, due to ER.
| as (km) | m + 1:m | Rs (m) | Shepherding |
|---|---|---|---|
| 314.7 | 4:3 | 540 | C1R inner edge |
| 348.2 | 8:7 | 420 | C1R inner edge |
| 364.1 (1) | 16:15 | 330 | C1R inner edge |
| 8:7 | 390 | C2R inner edge | |
| 366.0 (2) | 18:17 | 320 | C1R inner edge |
| 368.0 | 21:20 | 300 | C1R inner edge |
| 9:8 | 380 | C2R inner edge | |
| 407.7 (3) | 12:13 | 320 | C1R outer edge |
| 25:26 | 230 | C2R outer edge | |
| 408.6 | 23:24 | 240 | C2R outer edge |
| 415.8 (4) | 14:15 | 290 | C2R outer edge |
| 429.3 | 8:9 | 350 | C2R outer edge |
| 447.6 | 4:5 | 450 | C1R outer edge |
| 5:6 | 410 | C2R outer edge | |
Notes. From left to right are shown the semi-major axis as of the satellites, m + 1:m ER which they are involved in, their minimum radius Rs, and which edge they confine. The satellites that can simultaneously confine a C1R edge and a C2R edge are in italics. (1)This configuration is shown by the green dot in Fig. 7 (top panel). (2)This configuration is shown by the green dot in Fig. 7 (bottom panel). (3)This configuration is shown by the blue dot in Fig. 7 (top panel). (4)This configuration is shown by the blue dot in Figs. 7 (middle and bottom panels)
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