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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 16:30
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Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 09:32:00 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-30448
NORAD 57928 		4.755 14.35 2.7e-06
2026-10-13 06:11:43 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-38123
NORAD 100003 		4.783 14.44 2.6e-06
2026-10-15 01:47:06 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-35597
NORAD 66493 		4.957 14.21 2.6e-06
2026-10-13 18:17:03 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-32901
NORAD 62895 		4.890 14.36 2.6e-06
2026-10-15 14:17:33 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-31657
NORAD 59487 		4.973 14.35 2.5e-06
2026-10-15 22:40:17 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-32924
NORAD 63092 		4.600 14.95 2.4e-06
2026-10-14 17:48:04 STARLINK-5315
NORAD 55309 		SVYATOBOR 1 (RS60S)
NORAD 57187 		4.522 15.16 2.3e-06
2026-10-12 03:58:25 SVYATOBOR 1 (RS60S)
NORAD 57187 		COSMOS 2251 DEB
NORAD 40797 		0.931 15.14 1.8e-06
2026-10-14 08:01:24 SVYATOBOR 1 (RS60S)
NORAD 57187 		GALAPAGOS-UTE-SWSU
NORAD 67279 		2.423 1.08 7.5e-07
2026-10-16 22:56:17 SVYATOBOR 1 (RS60S)
NORAD 57187 		CZ-2C DEB
NORAD 37770 		2.230 13.31 5.0e-07
2026-10-17 07:31:00 SVYATOBOR 1 (RS60S)
NORAD 57187 		SITRO-AIS 7 (FARTUSHNIY)
NORAD 57194 		3.359 0.16 3.9e-07
2026-10-16 21:17:57 SVYATOBOR 1 (RS60S)
NORAD 57187 		SITRO-AIS 26
NORAD 59067 		4.237 4.68 2.4e-07
2026-10-12 23:31:23 SVYATOBOR 1 (RS60S)
NORAD 57187 		BANDWAGON-4 OBJECT M
NORAD 66304 		2.992 14.25 2.3e-07
2026-10-13 05:17:37 SVYATOBOR 1 (RS60S)
NORAD 57187 		SATMAR
NORAD 64551 		4.383 6.49 2.1e-07
2026-10-13 04:26:43 ION SCV-011
NORAD 56957 		SVYATOBOR 1 (RS60S)
NORAD 57187 		4.651 13.90 1.0e-07
2026-10-15 09:24:55 SVYATOBOR 1 (RS60S)
NORAD 57187 		STARLINK-35654
NORAD 66483 		4.751 13.76 1.0e-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.