Home›Maneuver Tracker›Close Approaches›YAOGAN-50 02 DEB ⟷ CZ-6A DEB
MediumProximity
Final forecastFinal forecast, made 17 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 8.93 km at 25 Oct 17:29 UTC. One of the two changed orbit around the time of the pass (a maneuver or strong drag), so this estimate is less certain.
Closest approach25 Oct 202617:29 UTC
Relative speed7.76 km/sat the closest approach
Altitude809 kmlow Earth orbit
Last confirmed25 Oct17:13 UTC · final forecast

CN YAOGAN-50 02 DEB and CN CZ-6A DEB were predicted to reach a closest approach of 7.72 km at 2026-10-25 17:29 UTC, at a relative speed of 7.76 km/s. Final forecast, made 17 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 8.93 km at 25 Oct 17:29 UTC. One of the two changed orbit around the time of the pass (a maneuver or strong drag), so this estimate is less certain. 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 100816
CountryPRC
Launched2026-03-15
COSPAR2026-051BL
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
CZ-6A DEBDebris
NORAD 54431
CountryPRC
Launched2022-11-11
COSPAR2022-151FF
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 · 809 KMISS 420Starlink 550

At 809 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 ⟷ CZ-6A DEB
2026-10-25 17:297.72 km Final forecast7.76 km/s809 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
28 Oct 06:23 UTC8.93 km Best estimate25 Oct 17:29 UTC26 Oct 09:16 UTCBest estimate
25 Oct 09:10 UTC7.72 km Forecast25 Oct 17:29 UTC24 Oct 05:43 UTCRe-check
25 Oct 08:51 UTC8.97 km Forecast25 Oct 17:29 UTC24 Oct 05:43 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
4.01 km10-29 10:45 UTC
YAOGAN-50 03CZ-6A DEB
7.20 km10-31 09:50 UTC
YAOGAN-50 02 DEBFENGYUN 1C DEB
7.20 km10-25 10:09 UTC
YAOGAN-50 02 DEBFENGYUN 1C 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 ⟷ CZ-6A DEB: 7.72 km predicted close approach”, https://orbitalradar.com/conjunction/100816-54431 (accessed 2026-10-30).