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 17:48:39 |
UNICORN-2L
NORAD 58727 |
OBJECT AF
NORAD 67277 |
0.381 | 0.19 | 3.0e-05 |
| 2026-10-13 00:02:47 |
STARLINK-3366
NORAD 51104 |
OBJECT AF
NORAD 67277 |
3.255 | 6.66 | 1.1e-05 |
| 2026-10-16 06:45:31 |
STARLINK-5265
NORAD 55317 |
OBJECT AF
NORAD 67277 |
3.070 | 14.99 | 5.3e-06 |
| 2026-10-11 08:13:20 |
STARLINK-3333
NORAD 50805 |
OBJECT AF
NORAD 67277 |
4.953 | 11.44 | 3.8e-06 |
| 2026-10-15 17:57:36 |
FORGESTAR-1
NORAD 64546 |
OBJECT AF
NORAD 67277 |
1.243 | 5.52 | 2.7e-06 |
| 2026-10-12 15:08:43 |
OBJECT AF
NORAD 67277 |
SL-3 DEB
NORAD 25655 |
1.115 | 10.60 | 2.7e-06 |
| 2026-10-15 18:18:46 |
OBJECT AF
NORAD 67277 |
EDDA-1
NORAD 69017 |
1.198 | 15.11 | 1.1e-06 |
| 2026-10-16 23:55:21 |
OBJECT C
NORAD 57168 |
OBJECT AF
NORAD 67277 |
3.084 | 1.27 | 4.6e-07 |
| 2026-10-12 13:09:22 |
AEROCUBE 18B
NORAD 63222 |
OBJECT AF
NORAD 67277 |
2.156 | 15.12 | 3.4e-07 |
| 2026-10-15 22:42:26 |
HORS 1
NORAD 57188 |
OBJECT AF
NORAD 67277 |
3.703 | 1.09 | 3.2e-07 |
| 2026-10-15 17:58:25 |
SITRO-AIS 26
NORAD 59067 |
OBJECT AF
NORAD 67277 |
4.599 | 5.64 | 2.0e-07 |
| 2026-10-17 01:02:10 |
OBJECT AF
NORAD 67277 |
JACKAL-004
NORAD 69012 |
3.096 | 15.09 | 1.6e-07 |
| 2026-10-16 14:17:09 |
YUNYAO-1 18
NORAD 58758 |
OBJECT AF
NORAD 67277 |
4.484 | 11.01 | 1.6e-07 |
| 2026-10-16 15:50:46 |
OBJECT AF
NORAD 67277 |
AZUR (GRS A)
NORAD 4221 |
3.957 | 14.69 | 1.3e-07 |
| 2026-10-12 12:48:26 |
COSMOS 2573
NORAD 58614 |
OBJECT AF
NORAD 67277 |
4.855 | 13.12 | 1.1e-07 |
| 2026-10-11 11:05:13 |
OBJECT AF
NORAD 67277 |
EYCORE-1
NORAD 69011 |
4.479 | 15.09 | 7.8e-08 |
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.