Conjunctions
Close approaches within 5 km between satellites in the portal catalog and other objects in orbit over the next seven days. The table is updated three times a day.
Last updated, UTC: 2026-10-11 00:30
Last updated, UTC: 2026-10-11 00:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-11 13:53:09 |
STARLINK-5621
NORAD 55434 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
2.691 | 13.20 | 1.0e-05 |
| 2026-10-15 05:39:19 |
STARLINK-5630
NORAD 55406 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
2.500 | 15.04 | 7.5e-06 |
| 2026-10-11 17:58:49 |
ION SCV-014
NORAD 62630 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
0.873 | 5.93 | 5.4e-06 |
| 2026-10-15 18:37:27 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
STARLINK-35498
NORAD 67017 |
3.359 | 14.42 | 5.2e-06 |
| 2026-10-15 10:39:00 |
STARLINK-34668
NORAD 64814 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
4.538 | 12.10 | 4.3e-06 |
| 2026-10-12 04:16:28 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
STARLINK-36093
NORAD 67015 |
4.075 | 13.87 | 4.1e-06 |
| 2026-10-14 09:14:22 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
STARLINK-36215
NORAD 67100 |
4.996 | 14.19 | 2.5e-06 |
| 2026-10-13 18:32:09 |
STARLINK-5605
NORAD 55411 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
4.750 | 14.98 | 2.1e-06 |
| 2026-10-11 18:06:46 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
3CAT-4
NORAD 60236 |
2.218 | 14.04 | 4.4e-07 |
| 2026-10-14 18:42:53 |
SITRO-AIS 14
NORAD 61752 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
3.358 | 9.23 | 3.2e-07 |
| 2026-10-16 05:00:27 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
SAUDISAT 1A (SO-41)
NORAD 26545 |
3.043 | 13.62 | 2.5e-07 |
| 2026-10-11 19:18:47 |
YAOGAN-30 11B
NORAD 49028 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
4.314 | 12.63 | 1.5e-07 |
| 2026-10-11 16:30:51 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
3CAT-4
NORAD 60236 |
4.213 | 14.05 | 1.2e-07 |
| 2026-10-15 01:03:30 |
LEMUR-2-LIA-MARTIN
NORAD 63248 |
LEMUR-2-LUCILLE-ROSE
NORAD 65403 |
4.613 | 13.84 | 1.1e-07 |
Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.