Home›Maneuver Tracker›Close Approaches›YAOGAN-31 J ⟷ ONEWEB-0606
MediumProximity
Final forecastFinal forecast, made 11 min before the pass.
Closest approach8 Nov 202602:32 UTC
Relative speed4.48 km/sat the closest approach
Altitude1,185 kmlow Earth orbit
Last confirmed8 Nov02:21 UTC · final forecast

CN YAOGAN-31 J and UK ONEWEB-0606 were predicted to reach a closest approach of 5.69 km at 2026-11-08 02:32 UTC, at a relative speed of 4.48 km/s. Final forecast, made 11 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 mattersBoth objects are catalogued as payloads. Screening continues as new element sets arrive; operators act on their own conjunction data.

The Two Objects

Dossiers from the satellite directory
NORAD 47695
CountryPRC
Launched2021-02-24
COSPAR2021-014E
Maneuver capableUnknown
NORAD 54670
CountryUK
Launched2022-12-08
COSPAR2022-166AE
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 1185 KMISS 420Starlink 550

At 1185 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

1 predicted pass under 10 km
Pair history · YAOGAN-31 J ⟷ ONEWEB-0606
2026-11-08 02:325.69 km Final forecast4.48 km/s1,185 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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 18:49 UTC5.69 km Forecast8 Nov 02:32 UTC7 Nov 16:26 UTCRe-check
7 Nov 12:51 UTC5.94 km Forecast8 Nov 02:32 UTC7 Nov 07:32 UTCRe-check
7 Nov 09:18 UTC6.50 km Forecast8 Nov 02:32 UTC7 Nov 05:56 UTCRe-check
7 Nov 03:54 UTC4.95 km Forecast8 Nov 02:32 UTC6 Nov 20:50 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
4.69 km11-10 02:15 UTC
YAOGAN-31 JCOSMOS 1275 DEB
5.91 km11-08 11:49 UTC
YAOGAN-31 JCOSMOS 397 DEB *
6.24 km11-04 14:56 UTC
YAOGAN-31 JQIANFAN-110

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 →