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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: 2026-10-12 00:30
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Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-14 03:42:52 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.158 0.01 2.5e-07
2026-10-14 05:18:13 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.262 0.01 2.4e-07
2026-10-15 01:08:45 NANOFF A
NORAD 58810 		SPACEMOBILE-010
NORAD 69591 		3.711 10.77 2.4e-07
2026-10-14 06:53:32 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.367 0.01 2.3e-07
2026-10-14 08:28:52 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.473 0.01 2.2e-07
2026-10-14 10:04:11 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.580 0.01 2.1e-07
2026-10-14 11:39:30 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.688 0.01 2.0e-07
2026-10-14 18:48:41 NANOFF A
NORAD 58810 		ROBUSTA-3A (MEDITERRANEE)
NORAD 60243 		3.145 14.52 1.9e-07
2026-10-14 13:14:49 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.797 0.01 1.9e-07
2026-10-12 18:11:58 NANOFF A
NORAD 58810 		CZ-6A DEB
NORAD 54553 		4.748 4.22 1.9e-07
2026-10-14 14:50:07 NANOFF B
NORAD 58755 		NANOFF A
NORAD 58810 		4.907 0.01 1.8e-07
2026-10-15 00:21:08 NANOFF A
NORAD 58810 		SPACEMOBILE-010
NORAD 69591 		4.278 10.79 1.8e-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.