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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
Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-14 12:17:54 STARLINK-5908
NORAD 55951
PIAST-M
NORAD 66758
2.949 11.17 1.1e-05
2026-10-12 15:12:43 MACSAT (FINCH 1)
NORAD 58024
PIAST-M
NORAD 66758
1.335 1.43 2.5e-06
2026-10-12 12:50:38 MACSAT (FINCH 1)
NORAD 58024
PIAST-M
NORAD 66758
2.058 1.43 1.0e-06
2026-10-13 13:55:39 CELTEE 1
NORAD 41850
PIAST-M
NORAD 66758
1.343 14.92 9.4e-07
2026-10-17 01:49:54 PIAST-M
NORAD 66758
AEPEX
NORAD 68506
1.947 12.71 7.2e-07
2026-10-13 09:18:29 TRANSPORTER-15 OBJECT CN
NORAD 66750
PIAST-M
NORAD 66758
2.527 0.01 6.6e-07
2026-10-16 11:34:14 CO3D 2
NORAD 64902
PIAST-M
NORAD 66758
3.106 0.68 4.6e-07
2026-10-13 15:40:30 BUGSAT-1 (TITA)
NORAD 40014
PIAST-M
NORAD 66758
3.568 3.63 3.4e-07
2026-10-12 16:47:26 MACSAT (FINCH 1)
NORAD 58024
PIAST-M
NORAD 66758
3.642 1.43 3.3e-07
2026-10-15 14:15:39 TRANSPORTER-15 OBJECT L
NORAD 66676
PIAST-M
NORAD 66758
3.700 0.08 3.2e-07
2026-10-13 09:58:48 CELTEE 1
NORAD 41850
PIAST-M
NORAD 66758
2.430 14.89 2.9e-07
2026-10-12 14:25:21 MACSAT (FINCH 1)
NORAD 58024
PIAST-M
NORAD 66758
3.969 1.43 2.8e-07
2026-10-16 08:23:54 PIAST-M
NORAD 66758
OBJECT C
NORAD 67748
3.806 7.07 2.7e-07
2026-10-12 22:56:59 HULIANWANG JISHU SHIYAN 6B
NORAD 63429
PIAST-M
NORAD 66758
3.075 13.33 2.6e-07
2026-10-13 15:30:23 CELTEE 1
NORAD 41850
PIAST-M
NORAD 66758
2.818 14.92 2.1e-07
2026-10-13 11:33:32 CELTEE 1
NORAD 41850
PIAST-M
NORAD 66758
3.209 14.89 1.6e-07
2026-10-13 18:46:43 KONDOR-FKA NO. 2
NORAD 62138
PIAST-M
NORAD 66758
4.113 13.68 1.4e-07
2026-10-12 04:00:11 PIAST-M
NORAD 66758
HULIANWANG JISHU SHIYAN 9C
NORAD 68833
4.912 13.41 1.0e-07
2026-10-13 12:20:54 CELTEE 1
NORAD 41850
PIAST-M
NORAD 66758
4.391 14.92 8.8e-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.