Home›Maneuver Tracker›Close Approaches›SJ-11-03 ⟷ FENGYUN 1C DEB
HighProximity
Final forecastFinal forecast, made 13 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 3.27 km at 3 Nov 19:59 UTC.
Closest approach3 Nov 202619:59 UTC
Relative speed14.42 km/sat the closest approach
Altitude686 kmlow Earth orbit
Last confirmed3 Nov19:46 UTC · final forecast

CN SJ-11-03 and CN FENGYUN 1C DEB were predicted to reach a closest approach of 3.35 km at 2026-11-03 19:59 UTC, at a relative speed of 14.42 km/s. Final forecast, made 13 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 3.27 km at 3 Nov 19:59 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
SJ-11-03Payload
NORAD 37730
CountryPRC
Launched2011-07-06
COSPAR2011-030A
Maneuver capableUnknown
NORAD 29856
CountryPRC
Launched1999-05-10
COSPAR1999-025FA
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 · 686 KMISS 420Starlink 550

At 686 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-11-03 ⟷ FENGYUN 1C DEB
2026-11-03 19:593.35 km Final forecast14.42 km/s686 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
7 Nov 06:54 UTC3.27 km Best estimate3 Nov 19:59 UTC3 Nov 19:17 UTCBest estimate
3 Nov 09:13 UTC3.35 km Forecast3 Nov 19:59 UTC2 Nov 21:52 UTCRe-check
2 Nov 22:30 UTC3.12 km Forecast3 Nov 19:59 UTC2 Nov 12:22 UTCRe-check
2 Nov 22:19 UTC6.09 km Forecast3 Nov 19:59 UTC2 Nov 12:22 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.12 km11-06 20:15 UTC
SJ-11-03ASTRO F DEB (LENS COVER)
3.09 km11-02 22:45 UTC
SJ-11-03IRIDIUM 33 DEB
3.14 km11-02 19:08 UTC
SJ-11-03COSMOS 2251 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 →