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 |
|---|---|---|---|---|---|
| 2026-10-14 16:19:57 |
SJ-9B
NORAD 38861 |
ICEYE-X78
NORAD 68995 |
0.723 | 10.11 | 6.6e-06 |
| 2026-10-14 17:06:49 |
SJ-9B
NORAD 38861 |
IO-1
NORAD 68498 |
1.279 | 3.05 | 2.6e-06 |
| 2026-10-14 23:34:33 |
SJ-9B
NORAD 38861 |
ICEYE-X78
NORAD 68995 |
1.194 | 10.08 | 2.4e-06 |
| 2026-10-13 07:01:05 |
SJ-9B
NORAD 38861 |
NOAA 16 DEB
NORAD 41348 |
1.031 | 14.94 | 1.5e-06 |
| 2026-10-13 16:59:08 |
SJ-9B
NORAD 38861 |
CUBY-3
NORAD 69875 |
1.794 | 9.74 | 1.1e-06 |
| 2026-10-14 09:52:13 |
SJ-9B
NORAD 38861 |
IO-1
NORAD 68498 |
2.332 | 3.06 | 8.0e-07 |
| 2026-10-15 06:47:04 |
SJ-9B
NORAD 38861 |
SL-14 R/B
NORAD 12988 |
2.405 | 14.77 | 7.1e-07 |
| 2026-10-13 19:24:06 |
SJ-9B
NORAD 38861 |
CUBY-3
NORAD 69875 |
2.597 | 9.77 | 5.2e-07 |
| 2026-10-15 06:13:31 |
SJ-9B
NORAD 38861 |
FENGYUN 1C DEB
NORAD 30569 |
2.054 | 14.86 | 3.9e-07 |
| 2026-10-11 16:58:54 |
SJ-9B
NORAD 38861 |
NOAA 16 DEB
NORAD 42374 |
2.535 | 14.93 | 2.5e-07 |
| 2026-10-16 10:09:17 |
SJ-9B
NORAD 38861 |
IRIDIUM 33 DEB
NORAD 35488 |
3.470 | 12.49 | 2.3e-07 |
| 2026-10-14 04:36:09 |
SJ-9B
NORAD 38861 |
CATCH-1
NORAD 60088 |
3.240 | 13.47 | 2.3e-07 |
| 2026-10-11 12:55:22 |
SJ-9B
NORAD 38861 |
NOAA 16 DEB
NORAD 41520 |
2.675 | 14.95 | 2.3e-07 |
| 2026-10-14 04:24:33 |
SJ-9B
NORAD 38861 |
SL-8 DEB
NORAD 15756 |
4.599 | 4.67 | 2.0e-07 |
| 2026-10-12 02:20:50 |
SJ-9B
NORAD 38861 |
CUBY-5
NORAD 69907 |
4.739 | 9.74 | 1.6e-07 |
| 2026-10-16 16:31:17 |
SJ-9B
NORAD 38861 |
FENGYUN 1C DEB
NORAD 37444 |
4.665 | 13.59 | 1.1e-07 |
| 2026-10-13 05:24:32 |
SJ-9B
NORAD 38861 |
NOAA 16 DEB
NORAD 41348 |
4.973 | 14.93 | 6.5e-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.