Home›Maneuver Tracker›Close Approaches›USA 32 DEB ⟷ IRIDIUM 120
HighProximity
Final forecastFinal forecast, made 17 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 2.85 km at 6 Nov 16:27 UTC.
Closest approach6 Nov 202616:27 UTC
Relative speed13.34 km/sat the closest approach
Altitude787 kmlow Earth orbit
Last confirmed6 Nov16:10 UTC · final forecast

US USA 32 DEB and US IRIDIUM 120 were predicted to reach a closest approach of 2.08 km at 2026-11-06 16:27 UTC, at a relative speed of 13.34 km/s. Final forecast, made 17 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 2.85 km at 6 Nov 16:27 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
NORAD 101048
CountryUS
Launched1988-09-05
COSPAR1988-078U
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
NORAD 42805
CountryUS
Launched2017-06-25
COSPAR2017-039C
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 787 KMISS 420Starlink 550

At 787 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 · USA 32 DEB ⟷ IRIDIUM 120
2026-11-06 18:072.13 km Final forecast · after: 1.25 km13.34 km/s787 kmView →
2026-11-06 16:272.08 km Final forecast · after: 2.85 km13.34 km/s787 kmShown above
2026-11-06 03:539.49 km Final forecast · after: 11.1 km13.38 km/s770 kmView →

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
10 Nov 13:53 UTC2.85 km Best estimate6 Nov 16:27 UTC6 Nov 17:18 UTCBest estimate
6 Nov 12:50 UTC2.08 km Forecast6 Nov 16:27 UTC6 Nov 09:13 UTCRe-check
6 Nov 08:55 UTC2.10 km Forecast6 Nov 16:27 UTC6 Nov 05:35 UTCRe-check
6 Nov 02:55 UTC671 m Forecast6 Nov 16:27 UTC5 Nov 21:16 UTCRe-check
5 Nov 17:07 UTC827 m Forecast6 Nov 16:27 UTC5 Nov 12:58 UTCRe-check
5 Nov 16:47 UTC956 m Forecast6 Nov 16:27 UTC5 Nov 12:58 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.20 km11-12 01:22 UTC
USA 32 DEBMETEOR 2-5 DEB
2.35 km11-05 07:55 UTC
USA 32 DEBDELTA 1 DEB
2.45 km11-06 19:02 UTC
USA 32 DEBFENGYUN 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 →