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: 2026-10-14 00:30
Last updated, UTC: 2026-10-14 00:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-16 16:11:06 |
RANDEV
NORAD 52898 |
IRIDIUM 33 DEB
NORAD 34521 |
1.467 | 15.02 | 6.9e-07 |
| 2026-10-16 21:41:10 |
RANDEV
NORAD 52898 |
FENGYUN 1C DEB
NORAD 32304 |
2.403 | 14.28 | 3.4e-07 |
| 2026-10-18 18:30:51 |
RANDEV
NORAD 52898 |
COSMOS 886 DEB
NORAD 9649 |
3.925 | 7.53 | 2.5e-07 |
| 2026-10-18 06:11:50 |
RANDEV
NORAD 52898 |
COSMOS 2251 DEB
NORAD 36385 |
2.651 | 14.92 | 2.2e-07 |
| 2026-10-16 23:17:04 |
RANDEV
NORAD 52898 |
DELTA 1 DEB
NORAD 13571 |
3.473 | 13.66 | 1.9e-07 |
| 2026-10-18 09:41:19 |
VNREDSAT 1
NORAD 39160 |
RANDEV
NORAD 52898 |
4.241 | 11.02 | 1.8e-07 |
| 2026-10-19 18:35:08 |
RANDEV
NORAD 52898 |
COSMOS 886 DEB
NORAD 9953 |
4.697 | 9.33 | 1.6e-07 |
| 2026-10-16 07:33:09 |
RANDEV
NORAD 52898 |
COSMOS 2251 DEB
NORAD 36540 |
3.997 | 13.07 | 1.6e-07 |
| 2026-10-18 13:12:18 |
RANDEV
NORAD 52898 |
FENGYUN 1C DEB
NORAD 31342 |
3.395 | 14.84 | 1.4e-07 |
| 2026-10-18 12:24:45 |
RANDEV
NORAD 52898 |
ORBCOMM FM115
NORAD 41186 |
3.800 | 14.16 | 1.4e-07 |
| 2026-10-18 20:11:08 |
RANDEV
NORAD 52898 |
COSMOS 2251 DEB
NORAD 33940 |
3.478 | 14.84 | 1.3e-07 |
| 2026-10-17 03:13:43 |
SWISSCUBE
NORAD 35932 |
RANDEV
NORAD 52898 |
4.328 | 13.21 | 1.3e-07 |
| 2026-10-17 11:13:18 |
RANDEV
NORAD 52898 |
SL-16 DEB
NORAD 22339 |
3.639 | 14.97 | 1.2e-07 |
| 2026-10-17 05:00:24 |
RANDEV
NORAD 52898 |
COSMOS 2251 DEB
NORAD 40810 |
4.898 | 13.75 | 9.3e-08 |
| 2026-10-14 15:55:50 |
AURA
NORAD 28376 |
RANDEV
NORAD 52898 |
4.764 | 14.83 | 7.1e-08 |
| 2026-10-18 06:50:46 |
RANDEV
NORAD 52898 |
COSMOS 2251 DEB
NORAD 34680 |
4.926 | 14.98 | 6.2e-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.