Home›Maneuver Tracker›Close Approaches›YAOGAN 9B ⟷ FENGYUN 1C DEB
MediumProximity
Final forecastFinal forecast, made 5 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 7.03 km at 21 Oct 10:51 UTC.
Closest approach21 Oct 202610:51 UTC
Relative speed9.48 km/sat the closest approach
Altitude1,040 kmlow Earth orbit
Last confirmed21 Oct10:46 UTC · final forecast

CN YAOGAN 9B and CN FENGYUN 1C DEB were predicted to reach a closest approach of 5.96 km at 2026-10-21 10:51 UTC, at a relative speed of 9.48 km/s. Final forecast, made 5 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 7.03 km at 21 Oct 10:51 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
YAOGAN 9BPayload
NORAD 36414
CountryPRC
Launched2010-03-05
COSPAR2010-009B
Maneuver capableUnknown
NORAD 35203
CountryPRC
Launched1999-05-10
COSPAR1999-025DPK
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 · 1040 KMISS 420Starlink 550

At 1040 km this pass sits inside the most congested band in low Earth orbit, home to the debris left by the 2007 ASAT test and the 2009 collision. 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 9B ⟷ FENGYUN 1C DEB
2026-10-21 10:515.96 km Final forecast9.48 km/s1,040 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
25 Oct 06:49 UTC7.03 km Best estimate21 Oct 10:51 UTC23 Oct 07:26 UTCBest estimate
21 Oct 09:46 UTC5.96 km Forecast21 Oct 10:51 UTC20 Oct 23:39 UTCRe-check
21 Oct 03:52 UTC5.98 km Forecast21 Oct 10:51 UTC20 Oct 14:44 UTCRe-check
20 Oct 12:32 UTC6.05 km Forecast21 Oct 10:51 UTC20 Oct 00:28 UTCRe-check
20 Oct 12:13 UTC6.01 km Forecast21 Oct 10:51 UTC19 Oct 17:20 UTCRe-check

These Objects Elsewhere

Other screened approaches · 7 days
4.06 km10-25 07:07 UTC
YAOGAN-31 CFENGYUN 1C DEB
8.70 km10-18 23:06 UTC
YAOGAN 9BFENGYUN 1C 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 9B ⟷ FENGYUN 1C DEB: 5.96 km predicted close approach”, https://orbitalradar.com/conjunction/35203-36414 (accessed 2026-10-25).