Home›Maneuver Tracker›Close Approaches›YAOGAN-50 02 DEB ⟷ SL-8 R/B
HighCross-border
Final forecastFinal forecast, made 17 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 2.94 km at 6 Nov 18:07 UTC.
Closest approach6 Nov 202618:07 UTC
Relative speed10.35 km/sat the closest approach
Altitude952 kmlow Earth orbit
Last confirmed6 Nov17:50 UTC · final forecast

CN YAOGAN-50 02 DEB and RU SL-8 R/B were predicted to reach a closest approach of 3.55 km at 2026-11-06 18:07 UTC, at a relative speed of 10.35 km/s. Final forecast, made 17 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 2.94 km at 6 Nov 18:07 UTC. This is a cross-border encounter between objects of different nations. 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 100803
CountryPRC
Launched2026-03-15
COSPAR2026-051AX
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
NORAD 14680
CountryCIS
Launched1984-02-02
COSPAR1984-010B
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 · 952 KMISS 420Starlink 550

At 952 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
2026-11-06 18:073.55 km Final forecast · after: 2.94 km10.35 km/s952 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
10 Nov 16:46 UTC2.94 km Best estimate6 Nov 18:07 UTC6 Nov 19:21 UTCBest estimate
6 Nov 08:55 UTC3.55 km Forecast6 Nov 18:07 UTC5 Nov 12:19 UTCRe-check
6 Nov 00:55 UTC7.61 km Forecast6 Nov 18:07 UTC4 Nov 22:40 UTCRe-check
6 Nov 00:35 UTC7.96 km Forecast6 Nov 18:07 UTC4 Nov 22:40 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.37 km11-10 21:40 UTC
YAOGAN-50SL-8 R/B
2.71 km11-13 07:44 UTC
YAOGAN-50 02 DEBSDA_1666
2.87 km11-08 06:58 UTC
YAOGAN-50 02 DEBSL-8 R/B

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 →