Home›Maneuver Tracker›Close Approaches›YAOGAN-39 04B ⟷ OBJECT A
HighProximity
Final forecastFinal forecast, made 15 min before the pass.
Closest approach31 Oct 202612:31 UTC
Relative speed13.09 km/sat the closest approach
Altitude514 kmlow Earth orbit
Last confirmed31 Oct12:16 UTC · final forecast

CN YAOGAN-39 04B and CN OBJECT A were predicted to reach a closest approach of 1.73 km at 2026-10-31 12:31 UTC, at a relative speed of 13.09 km/s. Final forecast, made 15 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 58143
CountryPRC
Launched2023-10-23
COSPAR2023-163C
Maneuver capableUnknown
OBJECT APayload
NORAD 61894
CountryPRC
Launched2024-11-11
COSPAR2024-205A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 514 KMISS 420Starlink 550

At 514 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-39 04B ⟷ OBJECT A
2026-10-31 12:311.73 km Final forecast13.09 km/s514 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
31 Oct 09:16 UTC1.73 km Forecast31 Oct 12:31 UTC31 Oct 04:27 UTCRe-check
30 Oct 21:09 UTC1.76 km Forecast31 Oct 12:31 UTC30 Oct 12:35 UTCRe-check
30 Oct 21:01 UTC2.53 km Forecast31 Oct 12:31 UTC29 Oct 23:39 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.28 km10-25 13:43 UTC
YAOGAN-39 04BOUT OF THE BOX
2.35 km10-26 11:04 UTC
YAOGAN-39 04BLUNA-2
2.39 km10-30 04:05 UTC
YAOGAN-39 04BOBJECT A

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-39 04B ⟷ OBJECT A: 1.73 km predicted close approach”, https://orbitalradar.com/conjunction/58143-61894 (accessed 2026-10-31).