Home›Maneuver Tracker›Close Approaches›YAOGAN-50 02 DEB ⟷ SL-8 R/B
HighCross-border
Final forecastFinal forecast, made minutes before the pass.
Closest approach23 Oct 202618:12 UTC
Relative speed7.26 km/sat the closest approach
Altitude962 kmlow Earth orbit
Last confirmed23 Oct18:09 UTC · final forecast

CN YAOGAN-50 02 DEB and RU SL-8 R/B were predicted to reach a closest approach of 3.29 km at 2026-10-23 18:12 UTC, at a relative speed of 7.26 km/s. Final forecast, made minutes before the pass. 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 each pass is re-checked every 20 minutes 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 100575
CountryPRC
Launched2026-03-15
COSPAR2026-051P
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
NORAD 13917
CountryCIS
Launched1983-03-24
COSPAR1983-021B
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 · 962 KMISS 420Starlink 550

At 962 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 predicted pass under 10 km
Pair history · YAOGAN-50 02 DEB ⟷ SL-8 R/B
2026-10-23 18:123.29 km Final forecast7.26 km/s962 kmShown above

Repeat encounters are common for objects in near-intersecting orbital planes. Each pass is re-screened as fresh element sets arrive; "Final forecast" means the screening still predicted it within 45 minutes of its time, "Not re-confirmed" means later screening stopped finding it.

Forecast Record

Every figure published for the pass shown above, newest first. Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.
Computed · figure · predicted time · orbit data · by
23 Oct 10:16 UTC3.29 km Forecast23 Oct 18:12 UTC22 Oct 21:34 UTCRe-check
22 Oct 21:42 UTC3.12 km Forecast23 Oct 18:12 UTC22 Oct 08:06 UTCRe-check
22 Oct 21:24 UTC4.56 km Forecast23 Oct 18:12 UTC22 Oct 08:06 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
3.33 km10-22 07:39 UTC
COSMOS 2233SL-8 R/B
5.70 km10-24 00:57 UTC
YAOGAN-50 02 DEBTHOR ABLESTAR DEB
6.21 km10-24 02:41 UTC
YAOGAN-50 02 DEBTHOR ABLESTAR DEB

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 — “YAOGAN-50 02 DEB ⟷ SL-8 R/B: 3.29 km predicted close approach”, https://orbitalradar.com/conjunction/100575-13917 (accessed 2026-10-24).