Home›Maneuver Tracker›Close Approaches›YAOGAN-50 02 DEB ⟷ SL-16 DEB
HighCross-border
Final forecastFinal forecast, made 14 min before the pass.
Closest approach21 Oct 202610:00 UTC
Relative speed14.28 km/sat the closest approach
Altitude884 kmlow Earth orbit
Last confirmed21 Oct09:46 UTC · final forecast

CN YAOGAN-50 02 DEB and RU SL-16 DEB were predicted to reach a closest approach of 4.02 km at 2026-10-21 10:00 UTC, at a relative speed of 14.28 km/s. Final forecast, made 14 min 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 100606
CountryPRC
Launched2026-03-15
COSPAR2026-051AW
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
SL-16 DEBDebris
NORAD 22223
CountryCIS
Launched1992-11-17
COSPAR1992-076E
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 884 KMISS 420Starlink 550

At 884 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-16 DEB
2026-10-21 10:004.02 km Final forecast14.28 km/s884 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
21 Oct 09:46 UTC4.02 km Forecast21 Oct 10:00 UTC21 Oct 02:07 UTCRe-check
21 Oct 03:52 UTC3.92 km Forecast21 Oct 10:00 UTC20 Oct 15:19 UTCRe-check
20 Oct 13:18 UTC3.89 km Forecast21 Oct 10:00 UTC20 Oct 07:17 UTCRe-check
20 Oct 12:58 UTC4.51 km Forecast21 Oct 10:00 UTC20 Oct 07:17 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
5.18 km10-21 00:09 UTC
YAOGAN-50 02 DEBNINGXIA-1 1
6.70 km10-17 07:08 UTC
YAOGAN-50 02 DEBSL-8 R/B
6.79 km10-21 02:11 UTC
YAOGAN-50 02 DEBCZ-6A 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 →

Cite this encounter: Orbital Radar — “YAOGAN-50 02 DEB ⟷ SL-16 DEB: 4.02 km predicted close approach”, https://orbitalradar.com/conjunction/100606-22223 (accessed 2026-10-22).