Home›Maneuver Tracker›Close Approaches›SJ-11-05 ⟷ FENGYUN 1C DEB
HighProximity
Final forecastFinal forecast, made minutes before the pass.
Closest approach29 Oct 202619:55 UTC
Drift speed325 m/s1,171 km/h, seen from FENGYUN 1C DEB
Altitude670 kmlow Earth orbit
Last confirmed29 Oct19:51 UTC · final forecast

CN SJ-11-05 and CN FENGYUN 1C DEB were predicted to reach a closest approach of 2.73 km at 2026-10-29 19:55 UTC, drifting past at about 325 m/s (1,171 km/h) as seen from FENGYUN 1C DEB. Final forecast, made minutes 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
SJ-11-05Payload
NORAD 39202
CountryPRC
Launched2013-07-15
COSPAR2013-035A
Maneuver capableUnknown
NORAD 31563
CountryPRC
Launched1999-05-10
COSPAR1999-025BZE
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 · 670 KMISS 420Starlink 550

At 670 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 · SJ-11-05 ⟷ FENGYUN 1C DEB
2026-10-29 19:552.73 km Final forecast0.33 km/s670 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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 00:15 UTC2.73 km Forecast29 Oct 19:55 UTC28 Oct 15:43 UTCRe-check
28 Oct 20:15 UTC1.73 km Forecast29 Oct 19:55 UTC27 Oct 23:20 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
669 m11-02 16:40 UTC
SJ-11-05COSMOS 2251 DEB
2.57 km10-31 18:42 UTC
SJ-11-05FENGYUN 1C DEB
3.29 km10-28 08:55 UTC
SJ-11-05FENGYUN 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 — “SJ-11-05 ⟷ FENGYUN 1C DEB: 2.73 km predicted close approach”, https://orbitalradar.com/conjunction/31563-39202 (accessed 2026-11-02).