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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: 2026-10-10 16:30
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Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 03:52:10 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		2.126 0.01 1.5e-05
2026-10-12 04:38:30 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		1.223 0.01 1.5e-05
2026-10-12 05:27:09 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		0.543 0.01 1.5e-05
2026-10-12 06:15:32 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		0.863 0.01 1.5e-05
2026-10-12 07:02:06 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		2.097 0.01 1.5e-05
2026-10-11 06:56:43 ANDURIL-216
NORAD 69879 		BOHR
NORAD 69917 		1.139 0.02 3.4e-06
2026-10-12 07:52:34 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		2.940 0.01 5.1e-07
2026-10-12 03:01:28 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		3.294 0.01 4.1e-07
2026-10-11 10:07:16 RCM-3
NORAD 44323 		BOHR
NORAD 69917 		3.230 12.04 2.8e-07
2026-10-12 08:36:59 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		4.106 0.01 2.6e-07
2026-10-12 02:17:11 BOHR
NORAD 69917 		LEMUR-2-DELOITTE-4
NORAD 69934 		4.128 0.01 2.6e-07
2026-10-15 14:46:18 COSMOS 2612
NORAD 68762 		BOHR
NORAD 69917 		3.545 12.86 2.1e-07
2026-10-12 01:22:40 BOHR
NORAD 69917 		PSLV DEB
NORAD 27089 		3.694 13.46 1.8e-07
2026-10-11 08:30:45 RCM-3
NORAD 44323 		BOHR
NORAD 69917 		4.129 12.04 1.7e-07
2026-10-11 11:43:48 RCM-3
NORAD 44323 		BOHR
NORAD 69917 		4.479 12.04 1.5e-07
2026-10-11 21:32:07 HUBBLE 6
NORAD 64562 		BOHR
NORAD 69917 		3.696 14.34 1.5e-07
2026-10-15 13:09:46 COSMOS 2612
NORAD 68762 		BOHR
NORAD 69917 		4.372 12.86 1.4e-07
2026-10-11 22:20:20 HUBBLE 6
NORAD 64562 		BOHR
NORAD 69917 		3.810 14.31 1.4e-07
2026-10-13 06:47:26 BOHR
NORAD 69917 		CZ-6A DEB
NORAD 56586 		4.377 14.96 8.3e-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.