HomeManeuver TrackerClose ApproachesUSA 25 ⟷ SL-8 R/B
high · CROSS-BORDER
8.65 kmmiss distance
Closest approach (TCA)
2026-09-13 07:27 UTC
Relative speed
13.99 km/s
Altitude
Current separation
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On 2026-09-13 07:27 UTC, US USA 25 and RU SL-8 R/B reached a closest approach (TCA) of 8.65 km, with a relative velocity of 13.99 km/s. This is a cross-border encounter between objects of different nations, the kind of event closely watched for space-security implications. 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 mattersOne side of this pass cannot maneuver, so any avoidance decision rests with the other operator. Screening continues as new element sets arrive.

The Two Objects

Dossiers from the satellite directory
USA 25Payload
NORAD 18025
CountryUS
Launched1987-05-15
COSPAR1987-043H
Maneuver capableUnknown
NORAD 12804
CountryCIS
Launched1981-09-04
COSPAR1981-087B
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 · 953 KMISS 420Starlink 550

At 953 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 · USA 25 ⟷ SL-8 R/B
Now8.65 km13.99 km/s953 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
4.84 km09-13 07:51 UTC
COSMOS 1559USA 25
6.58 km09-12 08:42 UTC
COSMOS 1275 DEBSL-8 R/B
7.04 km09-13 09:28 UTC
COSMOS 1640USA 25

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 — “USA 25 ⟷ SL-8 R/B: 8.65 km close approach”, https://orbitalradar.com/conjunction/12804-18025 (accessed 2026-09-15).