HomeManeuver TrackerClose ApproachesCOSMOS 1375 DEB ⟷ SL-8 R/B
medium · PROXIMITY
5.90 kmmiss distance
Closest approach (TCA)
2026-09-09 10:39 UTC
Relative speed
14.21 km/s
Altitude
Current separation
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On 2026-09-09 10:39 UTC, RU COSMOS 1375 DEB and RU SL-8 R/B reached a closest approach (TCA) of 5.90 km, with a relative velocity of 14.21 km/s. Miss distance and time of closest approach are computed by propagating the latest published orbital elements for both objects, and values update as new element sets are published. See the Satellite Maneuver Tracker for the live picture and space situational awareness for context.

Why it mattersNeither object can maneuver: the miss distance will evolve only with natural orbital perturbations, so screening continues until the pass is over.

The Two Objects

Dossiers from the satellite directory
NORAD 16375
CountryCIS
Launched1982-06-06
COSPAR1982-055P
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
NORAD 20805
CountryCIS
Launched1990-09-14
COSPAR1990-083B
Maneuver capableNo
Spent rocket stage: uncontrolled, tracked by the public catalogue.

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 959 KMISS 420Starlink 550

At 959 km this pass sits inside the most congested band in low Earth orbit, home to the debris left by the 2007 ASAT test and the 2009 collision. Objects here stay up for decades: there is too little atmospheric drag to clean the band naturally. Why crowded bands matter →

History Between This Pair

1 recorded pass under 10 km
Pair history · COSMOS 1375 DEB ⟷ SL-8 R/B
Now5.90 km14.21 km/s959 kmThis page

Repeat encounters are common for objects in near-intersecting orbital planes; each pass is re-screened as fresh element sets arrive.

These Objects Elsewhere

Other screened approaches · 7 days
5.11 km09-09 04:04 UTC
COSMOS 1275 DEBSL-8 R/B
8.09 km09-11 20:43 UTC
COSMOS 1375 DEBFENGYUN 1C DEB
8.16 km09-13 03:15 UTC
COSMOS 1375 DEBCOSMOS 1249 COOLANT

How These Numbers Are Computed

Miss distance and TCA come from propagating the latest published orbital elements for both objects and searching for the minimum separation over the screening window. Element sets carry kilometre-scale uncertainty, so figures here describe a close pass, not a collision prediction; a change in either object's published elements re-computes the pass automatically. What is a conjunction? → How conjunction assessment works →

Cite this encounter: Orbital Radar — “COSMOS 1375 DEB ⟷ SL-8 R/B: 5.90 km close approach”, https://orbitalradar.com/conjunction/16375-20805 (accessed 2026-09-15).