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 08:30
Last updated, UTC: 2026-10-11 08:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-14 18:32:11 |
STARLINK-38384
NORAD 100554 |
FLOCK 4Q-7
NORAD 58318 |
2.852 | 6.53 | 1.5e-05 |
| 2026-10-15 21:37:33 |
STARLINK-11210
NORAD 60116 |
FLOCK 4Q-7
NORAD 58318 |
2.132 | 14.83 | 1.2e-05 |
| 2026-10-14 04:09:38 |
STARLINK-38388
NORAD 100769 |
FLOCK 4Q-7
NORAD 58318 |
3.416 | 3.82 | 1.1e-05 |
| 2026-10-14 04:55:33 |
STARLINK-38388
NORAD 100769 |
FLOCK 4Q-7
NORAD 58318 |
3.909 | 3.82 | 8.5e-06 |
| 2026-10-14 17:46:18 |
STARLINK-38384
NORAD 100554 |
FLOCK 4Q-7
NORAD 58318 |
3.914 | 6.53 | 8.0e-06 |
| 2026-10-16 02:41:13 |
STARLINK-38352
NORAD 100542 |
FLOCK 4Q-7
NORAD 58318 |
4.197 | 5.98 | 7.1e-06 |
| 2026-10-16 04:37:38 |
STARLINK-11134
NORAD 59956 |
FLOCK 4Q-7
NORAD 58318 |
3.319 | 14.16 | 6.0e-06 |
| 2026-10-13 17:18:39 |
STARLINK-11139
NORAD 60402 |
FLOCK 4Q-7
NORAD 58318 |
4.709 | 9.60 | 4.9e-06 |
| 2026-10-16 06:55:17 |
STARLINK-11134
NORAD 59956 |
FLOCK 4Q-7
NORAD 58318 |
3.722 | 14.21 | 4.7e-06 |
| 2026-10-16 08:27:02 |
STARLINK-11134
NORAD 59956 |
FLOCK 4Q-7
NORAD 58318 |
3.788 | 14.22 | 4.6e-06 |
| 2026-10-15 20:51:39 |
STARLINK-11210
NORAD 60116 |
FLOCK 4Q-7
NORAD 58318 |
3.893 | 14.82 | 3.7e-06 |
| 2026-10-14 14:23:23 |
STARLINK-11134
NORAD 59956 |
FLOCK 4Q-7
NORAD 58318 |
4.538 | 13.78 | 3.5e-06 |
| 2026-10-14 10:33:57 |
STARLINK-11134
NORAD 59956 |
FLOCK 4Q-7
NORAD 58318 |
4.590 | 13.76 | 3.4e-06 |
| 2026-10-15 09:12:30 |
STARLINK-11102
NORAD 60065 |
FLOCK 4Q-7
NORAD 58318 |
4.407 | 14.74 | 2.9e-06 |
| 2026-10-16 20:01:59 |
SAMSAT-IONOSPHERE (RS75S)
NORAD 61784 |
FLOCK 4Q-7
NORAD 58318 |
3.018 | 14.45 | 2.2e-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.