Home›Maneuver Tracker›Close Approaches›YAOGAN-40 02A ⟷ FENGYUN 1C DEB
HighProximity
Final forecastFinal forecast, made 12 min before the pass.
Closest approach26 Oct 202615:59 UTC
Relative speed14.80 km/sat the closest approach
Altitude858 kmlow Earth orbit
Last confirmed26 Oct15:47 UTC · final forecast

CN YAOGAN-40 02A and CN FENGYUN 1C DEB were predicted to reach a closest approach of 2.90 km at 2026-10-26 15:59 UTC, at a relative speed of 14.80 km/s. Final forecast, made 12 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 63918
CountryPRC
Launched2025-05-11
COSPAR2025-096A
Maneuver capableUnknown
NORAD 30315
CountryPRC
Launched1999-05-10
COSPAR1999-025AAC
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 · 858 KMISS 420Starlink 550

At 858 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

3 predicted passes under 10 km
Pair history · YAOGAN-40 02A ⟷ FENGYUN 1C DEB
2026-10-27 00:288.17 km Live forecast14.80 km/s858 kmView →
2026-10-26 17:401.12 km Final forecast14.80 km/s858 kmView →
2026-10-26 15:592.90 km Final forecast14.80 km/s858 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
26 Oct 09:03 UTC2.90 km Forecast26 Oct 15:59 UTC25 Oct 23:38 UTCRe-check
25 Oct 21:23 UTC2.98 km Forecast26 Oct 15:59 UTC24 Oct 06:49 UTCRe-check
25 Oct 21:03 UTC9.60 km Forecast26 Oct 15:59 UTC24 Oct 06:49 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
283 m10-23 01:26 UTC
YAOGAN-40 02ASL-14 DEB
1.10 km10-26 17:41 UTC
YAOGAN-40 02BFENGYUN 1C DEB
2.06 km10-26 15:59 UTC
YAOGAN-40 02BFENGYUN 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-40 02A ⟷ FENGYUN 1C DEB: 2.90 km predicted close approach”, https://orbitalradar.com/conjunction/30315-63918 (accessed 2026-10-26).