Home›Maneuver Tracker›Close Approaches›YAOGAN 15 ⟷ ONEWEB-0534
medium · PROXIMITY
6.52 kmpredicted miss distance
Final forecastFinal forecast, made 5 min before the pass.
Predicted closest approach
2026-10-17 23:26 UTC
Relative speed
12.04 km/s
Altitude
Last confirmed
17 Oct 23:21 UTC
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CN YAOGAN 15 and UK ONEWEB-0534 were predicted to reach a closest approach of 6.52 km at 2026-10-17 23:26 UTC, at a relative speed of 12.04 km/s. Final forecast, made 5 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
YAOGAN 15Payload
NORAD 38354
CountryPRC
Launched2012-05-29
COSPAR2012-029A
Maneuver capableUnknown
NORAD 55797
CountryUK
Launched2023-03-09
COSPAR2023-029B
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 1176 KMISS 420Starlink 550

At 1176 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 15 ⟷ ONEWEB-0534
2026-10-17 23:266.52 km Final forecast12.04 km/s1,176 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.

These Objects Elsewhere

Other screened approaches · 7 days
933 m10-24 10:52 UTC
YAOGAN 15THOR ABLESTAR DEB
7.09 km10-24 05:13 UTC
YAOGAN 15ONEWEB-0147
7.17 km10-24 02:14 UTC
YAOGAN 15JASON 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 15 ⟷ ONEWEB-0534: 6.52 km predicted close approach”, https://orbitalradar.com/conjunction/38354-55797 (accessed 2026-10-24).