Home›Maneuver Tracker›Close Approaches›YAOGAN-42 02 ⟷ OBJECT B
HighProximity
Final forecastFinal forecast, made minutes before the pass.
Closest approach23 Oct 202600:18 UTC
Relative speed12.79 km/sat the closest approach
Altitude495 kmlow Earth orbit
Last confirmed23 Oct00:16 UTC · final forecast

CN YAOGAN-42 02 and CN OBJECT B were predicted to reach a closest approach of 4.17 km at 2026-10-23 00:18 UTC, at a relative speed of 12.79 km/s. Final forecast, made minutes 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 59557
CountryPRC
Launched2024-04-20
COSPAR2024-075A
Maneuver capableUnknown
OBJECT BPayload
NORAD 67747
CountryPRC
Launched2026-02-12
COSPAR2026-027B
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 495 KMISS 420Starlink 550

At 495 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-42 02 ⟷ OBJECT B
2026-10-23 00:184.17 km Final forecast12.79 km/s495 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
22 Oct 22:16 UTC4.17 km Forecast23 Oct 00:18 UTC22 Oct 09:51 UTCRe-check
22 Oct 11:50 UTC4.50 km Forecast23 Oct 00:18 UTC22 Oct 07:52 UTCRe-check
22 Oct 08:04 UTC3.88 km Forecast23 Oct 00:18 UTC21 Oct 20:48 UTCRe-check
22 Oct 02:04 UTC2.47 km Forecast23 Oct 00:18 UTC21 Oct 14:29 UTCRe-check
22 Oct 00:44 UTC3.53 km Forecast23 Oct 00:18 UTC21 Oct 06:35 UTCRe-check
22 Oct 00:24 UTC9.66 km Forecast23 Oct 00:18 UTC21 Oct 06:35 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.99 km10-22 20:52 UTC
YAOGAN-42 02IMPULSE-3 MIRA
4.23 km10-22 23:14 UTC
YAOGAN-42 02IMPULSE-3 MIRA
5.86 km10-23 04:01 UTC
OSIRIS-EOBJECT B

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-42 02 ⟷ OBJECT B: 4.17 km predicted close approach”, https://orbitalradar.com/conjunction/59557-67747 (accessed 2026-10-23).