Home›Maneuver Tracker›Close Approaches›YAOGAN-30 AD ⟷ CZ-6A DEB
MediumProximity
Final forecastFinal forecast, made 12 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 5.76 km at 24 Oct 19:01 UTC.
Closest approach24 Oct 202619:01 UTC
Relative speed13.94 km/sat the closest approach
Altitude558 kmlow Earth orbit
Last confirmed24 Oct18:49 UTC · final forecast

CN YAOGAN-30 AD and CN CZ-6A DEB were predicted to reach a closest approach of 5.76 km at 2026-10-24 19:01 UTC, at a relative speed of 13.94 km/s. Final forecast, made 12 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 5.76 km at 24 Oct 19:01 UTC. 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 49026
CountryPRC
Launched2021-07-19
COSPAR2021-065A
Maneuver capableUnknown
CZ-6A DEBDebris
NORAD 54638
CountryPRC
Launched2022-11-11
COSPAR2022-151PQ
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 · 558 KMISS 420Starlink 550

At 558 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 AD ⟷ CZ-6A DEB
2026-10-24 19:015.76 km Final forecast13.94 km/s558 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
27 Oct 08:24 UTC5.76 km Best estimate24 Oct 19:01 UTC24 Oct 05:21 UTCBest estimate
24 Oct 12:29 UTC5.76 km Forecast24 Oct 19:01 UTC24 Oct 05:21 UTCRe-check
24 Oct 06:29 UTC8.81 km Forecast24 Oct 19:01 UTC23 Oct 20:39 UTCRe-check
24 Oct 06:09 UTC8.90 km Forecast24 Oct 19:01 UTC23 Oct 20:39 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
3.49 km10-27 19:30 UTC
YAOGAN-30 ADELECTRON KICK STAGE R/B
4.75 km10-26 11:12 UTC
YAOGAN-30 ADRISAT-2BR2
6.79 km10-28 06:43 UTC
YAOGAN-30 ADOBJECT H

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 AD ⟷ CZ-6A DEB: 5.76 km predicted close approach”, https://orbitalradar.com/conjunction/49026-54638 (accessed 2026-10-28).