Home›Maneuver Tracker›Close Approaches›YAOGAN 11 ⟷ CZ-6A DEB
MediumProximity
Final forecastFinal forecast, made 19 min before the pass.
Closest approach8 Nov 202600:01 UTC
Relative speed14.16 km/sat the closest approach
Altitude594 kmlow Earth orbit
Last confirmed7 Nov23:41 UTC · final forecast

CN YAOGAN 11 and CN CZ-6A DEB were predicted to reach a closest approach of 9.04 km at 2026-11-08 00:01 UTC, at a relative speed of 14.16 km/s. Final forecast, made 19 min before the pass. 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 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
YAOGAN 11Payload
NORAD 37165
CountryPRC
Launched2010-09-22
COSPAR2010-047A
Maneuver capableUnknown
CZ-6A DEBDebris
NORAD 55231
CountryPRC
Launched2022-11-11
COSPAR2022-151WY
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 · 594 KMISS 420Starlink 550

At 594 km this pass sits in low Earth orbit. 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

6 predicted passes under 10 km
Pair history · YAOGAN 11 ⟷ CZ-6A DEB
2026-11-09 04:228.95 km Final forecast14.04 km/s653 kmView →
2026-11-09 01:073.26 km Final forecast14.04 km/s653 kmView →
2026-11-08 23:301.71 km Final forecast14.04 km/s653 kmView →
2026-11-08 20:156.66 km Final forecast14.04 km/s653 kmView →
2026-11-08 17:018.12 km Withdrawn14.04 km/s653 kmView →
2026-11-08 00:019.04 km Final forecast14.16 km/s594 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
7 Nov 12:51 UTC9.04 km Forecast8 Nov 00:01 UTC7 Nov 04:03 UTCRe-check
7 Nov 12:11 UTC8.87 km Forecast8 Nov 00:01 UTC6 Nov 21:35 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.28 km11-04 08:21 UTC
YAOGAN 11SL-8 DEB *
1.32 km11-08 07:57 UTC
YAOGAN 11UPM/LBSAT
1.52 km11-03 23:26 UTC
FIRESAT3CZ-6A 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 →