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 |
|---|---|---|---|---|---|
| 2026-10-11 17:07:03 |
LEMUR-2-HUBBLE-4
NORAD 64565 |
ET-001C
NORAD 69942 |
0.630 | 14.35 | 5.0e-06 |
| 2026-10-12 15:06:20 |
FORMOSAT-7R (TRITON)
NORAD 58017 |
ET-001C
NORAD 69942 |
0.806 | 14.98 | 2.4e-06 |
| 2026-10-13 16:24:36 |
ET-001C
NORAD 69942 |
ELISA E12
NORAD 38010 |
2.210 | 13.19 | 5.1e-07 |
| 2026-10-16 06:38:15 |
OBJECT A
NORAD 51946 |
ET-001C
NORAD 69942 |
3.460 | 5.87 | 3.4e-07 |
| 2026-10-16 16:03:11 |
PERSEUS-M1
NORAD 40039 |
ET-001C
NORAD 69942 |
3.492 | 6.03 | 3.4e-07 |
| 2026-10-16 06:23:50 |
AE1A
NORAD 68487 |
ET-001C
NORAD 69942 |
3.883 | 7.25 | 2.6e-07 |
| 2026-10-12 10:48:41 |
ION SCV-018
NORAD 64575 |
ET-001C
NORAD 69942 |
3.068 | 14.29 | 2.1e-07 |
| 2026-10-13 12:23:19 |
ET-001C
NORAD 69942 |
ELISA E12
NORAD 38010 |
3.543 | 13.22 | 2.0e-07 |
| 2026-10-14 11:48:27 |
HODOYOSHI-4
NORAD 40011 |
ET-001C
NORAD 69942 |
4.270 | 9.59 | 1.9e-07 |
| 2026-10-13 18:01:07 |
ET-001C
NORAD 69942 |
ELISA E12
NORAD 38010 |
3.992 | 13.19 | 1.6e-07 |
| 2026-10-15 09:56:37 |
CONNECTA IOT-5
NORAD 62703 |
ET-001C
NORAD 69942 |
3.241 | 14.99 | 1.5e-07 |
| 2026-10-17 00:49:59 |
ET-001C
NORAD 69942 |
YAOGAN-29 DEB
NORAD 42673 |
3.836 | 13.91 | 1.5e-07 |
| 2026-10-15 21:29:06 |
ET-001C
NORAD 69942 |
SL-16 DEB
NORAD 22327 |
4.185 | 13.64 | 1.3e-07 |
| 2026-10-13 20:59:00 |
CAPELLA-16 (ACADIA-6)
NORAD 65318 |
ET-001C
NORAD 69942 |
3.979 | 14.97 | 1.0e-07 |
| 2026-10-12 13:29:46 |
FORMOSAT-7R (TRITON)
NORAD 58017 |
ET-001C
NORAD 69942 |
4.996 | 14.98 | 6.3e-08 |
| 2026-10-12 16:42:54 |
FORMOSAT-7R (TRITON)
NORAD 58017 |
ET-001C
NORAD 69942 |
4.998 | 14.98 | 6.3e-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.