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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
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Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 05:35:08 GRUS-1E
NORAD 47935 		STARLINK-5494
NORAD 55650 		4.300 15.01 2.6e-06
2026-10-14 00:35:24 GRUS-1E
NORAD 47935 		STARLINK-36173
NORAD 67210 		4.521 15.05 2.3e-06
2026-10-13 14:03:19 GRUS-1E
NORAD 47935 		STARLINK-5423
NORAD 55670 		4.611 14.98 2.3e-06
2026-10-13 08:36:52 GRUS-1E
NORAD 47935 		STARLINK-36216
NORAD 67217 		4.861 15.06 2.0e-06
2026-10-16 23:45:47 GRUS-1E
NORAD 47935 		HAWK-10B
NORAD 60545 		1.607 14.93 6.3e-07
2026-10-16 13:18:50 GRUS-1E
NORAD 47935 		GNOMES-5
NORAD 60574 		1.845 14.84 5.0e-07
2026-10-13 09:05:56 GRUS-1E
NORAD 47935 		COSMOS 2251 DEB
NORAD 34327 		3.595 12.57 2.1e-07
2026-10-12 15:17:35 GRUS-1E
NORAD 47935 		IRIDIUM 33 DEB
NORAD 33960 		4.916 3.16 1.8e-07
2026-10-12 03:00:52 GRUS-1E
NORAD 47935 		FALCON 1 R/B
NORAD 35579 		4.070 12.10 1.8e-07
2026-10-11 12:10:45 GRUS-1E
NORAD 47935 		IRIDIUM 33 DEB
NORAD 34091 		3.824 13.18 1.7e-07
2026-10-15 16:25:31 GRUS-1E
NORAD 47935 		CZ-6A DEB
NORAD 54638 		3.433 14.47 1.6e-07
2026-10-13 02:01:22 GRUS-1E
NORAD 47935 		UM5-RIBAT
NORAD 60554 		3.278 14.87 1.6e-07
2026-10-16 18:42:17 GRUS-1E
NORAD 47935 		SHIYAN-24C 02
NORAD 58651 		4.968 9.91 1.4e-07
2026-10-14 18:59:55 FORMOSAT 7-1
NORAD 44349 		GRUS-1E
NORAD 47935 		4.612 12.76 1.3e-07
2026-10-14 19:59:57 GRUS-1E
NORAD 47935 		GNOMES-4
NORAD 58462 		4.017 14.99 9.9e-08
2026-10-16 10:56:23 GRUS-1E
NORAD 47935 		HAWK-10A
NORAD 60540 		4.336 14.91 8.7e-08
2026-10-12 07:37:59 GRUS-1E
NORAD 47935 		TORO
NORAD 60530 		4.432 14.93 8.3e-08
2026-10-13 16:12:36 GRUS-1E
NORAD 47935 		PEGASUS DEB
NORAD 25445 		4.444 15.17 7.5e-08
2026-10-14 10:14:13 GRUS-1E
NORAD 47935 		SKYCRAFT-4A
NORAD 64897 		4.601 15.02 7.4e-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.