Home›Maneuver Tracker›Close Approaches›YAOGAN-40 04A ⟷ FENGYUN 1C DEB
high · PROXIMITY
4.88 kmpredicted miss distance
Not re-confirmedLast confirmed 6 h before the pass. Later screening did not re-confirm it.
Predicted closest approach
2026-10-17 15:31 UTC
Relative speed
5.21 km/s
Altitude
Last confirmed
17 Oct 09:38 UTC
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CN YAOGAN-40 04A and CN FENGYUN 1C DEB were predicted to reach a closest approach of 4.88 km at 2026-10-17 15:31 UTC, at a relative speed of 5.21 km/s. Screening last confirmed this pass 6 h before it was due and did not re-confirm it after that, so the figure may have been overtaken by newer orbital data, for example after a maneuver. 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 100823
CountryPRC
Launched2026-09-24
COSPAR2026-222A
Maneuver capableUnknown
NORAD 30120
CountryPRC
Launched1999-05-10
COSPAR1999-025RZ
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 · 773 KMISS 420Starlink 550

At 773 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-40 04A ⟷ FENGYUN 1C DEB
2026-10-17 15:314.88 km Not re-confirmed5.21 km/s773 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.

These Objects Elsewhere

Other screened approaches · 7 days
1.79 km10-21 05:50 UTC
YAOGAN-40 04ANOAA 16 DEB
2.83 km10-20 20:24 UTC
YAOGAN-40 04ACOSMOS 1867 COOLANT
2.96 km10-19 05:56 UTC
YAOGAN-40 04ACZ-6A 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 04A ⟷ FENGYUN 1C DEB: 4.88 km forecast, not re-confirmed”, https://orbitalradar.com/conjunction/100823-30120 (accessed 2026-10-20).