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: 2026-10-10 16:30
Last updated, UTC: 2026-10-10 16:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-12 05:48:43 |
SNUSAT-2
NORAD 43782 |
STARLINK-1417
NORAD 45693 |
2.370 | 14.66 | 1.0e-05 |
| 2026-10-12 04:32:19 |
SNUSAT-2
NORAD 43782 |
STARLINK-1276
NORAD 45368 |
4.442 | 10.05 | 5.3e-06 |
| 2026-10-13 07:21:22 |
SNUSAT-2
NORAD 43782 |
HULIANWANG JISHU SHIYAN 9D
NORAD 68834 |
1.481 | 12.67 | 1.2e-06 |
| 2026-10-16 04:51:11 |
SNUSAT-2
NORAD 43782 |
IOD-2
NORAD 64538 |
1.976 | 7.78 | 9.9e-07 |
| 2026-10-14 10:30:42 |
SNUSAT-2
NORAD 43782 |
SPACEMOBILE-001
NORAD 61047 |
2.433 | 14.05 | 3.7e-07 |
| 2026-10-12 07:51:57 |
SNUSAT-2
NORAD 43782 |
DRUMS
NORAD 49401 |
3.896 | 2.33 | 2.9e-07 |
| 2026-10-15 22:42:12 |
SNUSAT-2
NORAD 43782 |
BSLT-3
NORAD 69009 |
2.717 | 14.77 | 2.4e-07 |
| 2026-10-12 04:43:23 |
ASNARO-2
NORAD 43152 |
SNUSAT-2
NORAD 43782 |
4.193 | 5.96 | 2.3e-07 |
| 2026-10-12 10:12:22 |
SNUSAT-2
NORAD 43782 |
GOOD ANCESTOR KILAKILA
NORAD 64528 |
4.397 | 7.91 | 2.0e-07 |
| 2026-10-13 20:13:42 |
KANOPUS-V 3
NORAD 43180 |
SNUSAT-2
NORAD 43782 |
3.308 | 14.54 | 1.8e-07 |
| 2026-10-13 21:55:59 |
SNUSAT-2
NORAD 43782 |
COSMOS 397 DEB
NORAD 5012 |
4.955 | 5.20 | 1.7e-07 |
| 2026-10-16 23:09:48 |
SNUSAT-2
NORAD 43782 |
DROID.002
NORAD 63223 |
3.461 | 14.87 | 1.4e-07 |
| 2026-10-16 21:35:14 |
SNUSAT-2
NORAD 43782 |
DROID.002
NORAD 63223 |
4.068 | 14.87 | 1.0e-07 |
| 2026-10-17 00:44:23 |
SNUSAT-2
NORAD 43782 |
DROID.002
NORAD 63223 |
4.251 | 14.87 | 9.5e-08 |
| 2026-10-15 21:54:52 |
SNUSAT-2
NORAD 43782 |
BSLT-3
NORAD 69009 |
4.667 | 14.75 | 8.2e-08 |
| 2026-10-11 08:21:05 |
SNUSAT-2
NORAD 43782 |
SELENE
NORAD 69020 |
4.722 | 14.77 | 8.0e-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.