Home›Maneuver Tracker›Close Approaches›YAOGAN-30 V ⟷ CZ-4 DEB
CriticalProximity
Final forecastFinal forecast, made 5 min before the pass.
Closest approach29 Oct 202622:36 UTC
Relative speed7.86 km/sat the closest approach
Altitude556 kmlow Earth orbit
Last confirmed29 Oct22:31 UTC · final forecast

CN YAOGAN-30 V and CN CZ-4 DEB were predicted to reach a closest approach of 618 m at 2026-10-29 22:36 UTC, at a relative speed of 7.86 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 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
NORAD 46808
CountryPRC
Launched2020-10-26
COSPAR2020-076B
Maneuver capableUnknown
CZ-4 DEBDebris
NORAD 35375
CountryPRC
Launched2006-10-23
COSPAR2006-046H
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 · 556 KMISS 420Starlink 550

At 556 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-30 V ⟷ CZ-4 DEB
2026-10-29 22:36618 m Final forecast7.86 km/s556 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
29 Oct 21:31 UTC618 m Forecast29 Oct 22:36 UTC29 Oct 06:39 UTCRe-check
29 Oct 09:31 UTC931 m Forecast29 Oct 22:36 UTC28 Oct 13:07 UTCRe-check
29 Oct 09:12 UTC5.32 km Forecast29 Oct 22:36 UTC28 Oct 13:07 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
736 m10-27 18:05 UTC
YAOGAN-30 VLEMUR 2 STAR-FOX
1.22 km10-27 08:22 UTC
RASSVET-3 20CZ-4 DEB
1.63 km11-03 04:22 UTC
YAOGAN-30 VQPS-SAR-9 SUSANOO-I

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-30 V ⟷ CZ-4 DEB: 618 m predicted close approach”, https://orbitalradar.com/conjunction/35375-46808 (accessed 2026-11-02).