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 08:30
Last updated, UTC: 2026-10-11 08:30
| Time of closest approach, UTC | Object 1 | Object 2 | Distance, km | Speed, km/s | Max. probability |
|---|---|---|---|---|---|
| 2026-10-11 16:44:15 |
HORUS 1
NORAD 55690 |
STARLINK-5579
NORAD 55746 |
1.801 | 8.37 | 3.5e-05 |
| 2026-10-17 10:41:04 |
HORUS 1
NORAD 55690 |
FLOCK 4H-1
NORAD 66704 |
0.881 | 0.02 | 5.7e-06 |
| 2026-10-12 19:50:30 |
HORUS 1
NORAD 55690 |
HERMES-6
NORAD 63489 |
0.740 | 15.10 | 2.9e-06 |
| 2026-10-13 08:37:22 |
HORUS 1
NORAD 55690 |
LPNTSAT-002 (IOD-2)
NORAD 68409 |
1.008 | 14.98 | 1.6e-06 |
| 2026-10-13 05:09:51 |
HORUS 1
NORAD 55690 |
YAOGAN-43 01E
NORAD 60462 |
1.601 | 13.36 | 9.7e-07 |
| 2026-10-15 20:47:52 |
HORUS 1
NORAD 55690 |
IRIDE-MS1-EAGLET 2-2
NORAD 66696 |
3.090 | 0.04 | 4.6e-07 |
| 2026-10-12 18:15:56 |
HORUS 1
NORAD 55690 |
HERMES-6
NORAD 63489 |
2.131 | 15.10 | 3.4e-07 |
| 2026-10-13 00:23:11 |
KANOPUS-V 4
NORAD 43181 |
HORUS 1
NORAD 55690 |
2.684 | 15.04 | 2.2e-07 |
| 2026-10-11 20:36:23 |
HORUS 1
NORAD 55690 |
CZ-4C R/B
NORAD 41039 |
4.424 | 0.11 | 2.2e-07 |
| 2026-10-13 03:35:20 |
HORUS 1
NORAD 55690 |
YAOGAN-43 01E
NORAD 60462 |
3.525 | 13.38 | 2.0e-07 |
| 2026-10-11 12:56:13 |
HORUS 1
NORAD 55690 |
YAOGAN-39 01A
NORAD 57727 |
3.960 | 12.70 | 1.7e-07 |
| 2026-10-13 02:45:06 |
KANOPUS-V 4
NORAD 43181 |
HORUS 1
NORAD 55690 |
3.388 | 15.02 | 1.4e-07 |
| 2026-10-13 04:19:43 |
KANOPUS-V 4
NORAD 43181 |
HORUS 1
NORAD 55690 |
3.506 | 15.02 | 1.3e-07 |
| 2026-10-12 13:24:22 |
FGRST (GLAST)
NORAD 33053 |
HORUS 1
NORAD 55690 |
4.765 | 12.16 | 1.3e-07 |
| 2026-10-12 21:25:03 |
HORUS 1
NORAD 55690 |
HERMES-6
NORAD 63489 |
3.611 | 15.10 | 1.2e-07 |
| 2026-10-12 22:48:34 |
KANOPUS-V 4
NORAD 43181 |
HORUS 1
NORAD 55690 |
4.702 | 15.04 | 7.3e-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.