Home›Maneuver Tracker›Close Approaches›DRAGON GRACE 2 ⟷ FENGYUN 1C DEB
HighCross-border
Final forecastFinal forecast, made 20 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 11.8 km at 29 Oct 08:34 UTC.
Closest approach29 Oct 202608:34 UTC
Relative speed13.62 km/sat the closest approach
Altitude422 kmlow Earth orbit
Last confirmed29 Oct08:15 UTC · final forecast

US DRAGON GRACE 2 and CN FENGYUN 1C DEB were predicted to reach a closest approach of 6.74 km at 2026-10-29 08:34 UTC, at a relative speed of 13.62 km/s. Final forecast, made 20 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 11.8 km at 29 Oct 08:34 UTC. This is a cross-border encounter between objects of different nations, the kind of event closely watched for space-security implications. 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 100882
CountryUS
Launched2026-10-01
COSPAR2026-226A
Maneuver capableUnknown
NORAD 36225
CountryPRC
Launched1999-05-10
COSPAR1999-025DVA
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 · 422 KMISS 420Starlink 550

At 422 km this pass sits in low Earth orbit. 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 · DRAGON GRACE 2 ⟷ FENGYUN 1C DEB
2026-11-04 04:527.29 km Live forecast14.70 km/s424 kmView →
2026-11-04 04:064.14 km Live forecast14.71 km/s419 kmView →
2026-10-29 08:346.74 km Final forecast13.62 km/s422 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
2 Nov 07:27 UTC11.84 km Best estimate29 Oct 08:34 UTC29 Oct 07:35 UTCBest estimate
29 Oct 00:15 UTC6.74 km Forecast29 Oct 08:34 UTC28 Oct 11:12 UTCRe-check
28 Oct 10:48 UTC5.36 km Forecast29 Oct 08:34 UTC27 Oct 05:54 UTCRe-check
28 Oct 10:28 UTC5.94 km Forecast29 Oct 08:34 UTC27 Oct 05:54 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.09 km10-31 20:15 UTC
DRAGON GRACE 2TIANHUI 4B
2.81 km10-29 11:23 UTC
DRAGON GRACE 2FLOCK 4BE-1
3.55 km11-03 16:15 UTC
DRAGON GRACE 2CZ-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 →