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 16:30
Last updated, UTC: 2026-10-11 16:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-12 19:07:56 |
STARLINK-4506
NORAD 53554 |
ICEYE-X60
NORAD 66753 |
0.163 | 14.67 | 2.1e-03 |
| 2026-10-17 06:50:13 |
STARLINK-35043
NORAD 65436 |
ICEYE-X60
NORAD 66753 |
1.578 | 14.14 | 2.6e-05 |
| 2026-10-16 23:45:33 |
OBJECT A
NORAD 59810 |
ICEYE-X60
NORAD 66753 |
0.629 | 1.06 | 1.1e-05 |
| 2026-10-17 09:13:20 |
STARLINK-35043
NORAD 65436 |
ICEYE-X60
NORAD 66753 |
2.836 | 14.11 | 8.0e-06 |
| 2026-10-12 19:55:39 |
STARLINK-4506
NORAD 53554 |
ICEYE-X60
NORAD 66753 |
3.746 | 14.67 | 3.9e-06 |
| 2026-10-13 00:45:15 |
STARLINK-5288
NORAD 55307 |
ICEYE-X60
NORAD 66753 |
3.641 | 15.10 | 3.5e-06 |
| 2026-10-14 12:54:42 |
ICEYE-X60
NORAD 66753 |
OBJECT J
NORAD 67001 |
1.140 | 0.76 | 3.4e-06 |
| 2026-10-17 07:37:55 |
STARLINK-35043
NORAD 65436 |
ICEYE-X60
NORAD 66753 |
4.395 | 14.11 | 3.3e-06 |
| 2026-10-15 21:46:46 |
STARLINK-4505
NORAD 53556 |
ICEYE-X60
NORAD 66753 |
4.310 | 14.44 | 3.2e-06 |
| 2026-10-12 14:48:45 |
ICEYE-X60
NORAD 66753 |
OBJECT D
NORAD 43761 |
3.570 | 4.21 | 3.3e-07 |
| 2026-10-14 13:44:00 |
ICEYE-X60
NORAD 66753 |
FENGYUN 1C DEB
NORAD 32350 |
3.665 | 3.25 | 3.2e-07 |
| 2026-10-15 11:58:05 |
ICEYE-X60
NORAD 66753 |
NEONSAT-1A
NORAD 67614 |
3.786 | 6.06 | 2.9e-07 |
| 2026-10-16 22:57:50 |
OBJECT A
NORAD 59810 |
ICEYE-X60
NORAD 66753 |
4.060 | 1.07 | 2.7e-07 |
| 2026-10-17 08:25:33 |
ICEYE-X60
NORAD 66753 |
CZ-6A R/B
NORAD 52152 |
2.913 | 14.10 | 2.5e-07 |
| 2026-10-15 22:20:03 |
ICEYE-X60
NORAD 66753 |
CZ-4B DEB
NORAD 44593 |
4.157 | 4.95 | 2.4e-07 |
| 2026-10-16 20:44:57 |
ICEYE-X60
NORAD 66753 |
FENGYUN 1C DEB
NORAD 31536 |
3.255 | 14.87 | 1.6e-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.