Home›Maneuver Tracker›Close Approaches›USA 486 ⟷ OBJECT AD
HighProximity
Final forecastFinal forecast, made 19 min before the pass.
Closest approach10 Nov 202619:26 UTC
Relative speed10.62 km/sat the closest approach
Altitude365 kmlow Earth orbit
Last confirmed10 Nov19:06 UTC · final forecast

US USA 486 and TBD OBJECT AD were predicted to reach a closest approach of 1.21 km at 2026-11-10 19:26 UTC, at a relative speed of 10.62 km/s. Final forecast, made 19 min 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 mattersBoth objects are catalogued as payloads. Screening continues as new element sets arrive; operators act on their own conjunction data.

The Two Objects

Dossiers from the satellite directory
USA 486Payload
NORAD 62757
CountryUS
Launched2025-01-21
COSPAR2025-014Y
Maneuver capableUnknown
OBJECT ADPayload
NORAD 62404
CountryTBD
Launched2024-12-21
COSPAR2024-247AD
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 365 KMISS 420Starlink 550

At 365 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

1 predicted pass under 10 km
Pair history · USA 486 ⟷ OBJECT AD
2026-11-10 19:261.21 km Final forecast10.62 km/s365 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
10 Nov 14:46 UTC1.21 km Forecast10 Nov 19:26 UTC10 Nov 00:21 UTCRe-check
10 Nov 14:28 UTC1.72 km Forecast10 Nov 19:26 UTC10 Nov 00:21 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.15 km11-11 23:38 UTC
USA 486RASSVET-3 26
4.36 km11-11 16:13 UTC
USA 486STARLINK-11154 [DTC]
5.02 km11-11 08:50 UTC
USA 486STARLINK-11728 [DTC]

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 →