Home›Maneuver Tracker›Close Approaches›YAOGAN-40 04A ⟷ ADEOS 2
HighProximity
Live forecastConfirmed by the latest screening, 12 Nov 12:48 UTC.
Closest approach13 Nov 202608:38 UTC
Relative speed13.51 km/sat the closest approach
Altitude802 kmlow Earth orbit
Separation now—live

CN YAOGAN-40 04A and JP ADEOS 2 are predicted to reach a closest approach of 1.66 km at 2026-11-13 08:38 UTC, at a relative speed of 13.51 km/s. Confirmed by the latest screening, 12 Nov 12:48 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 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
NORAD 100823
CountryPRC
Launched2026-09-24
COSPAR2026-222A
Maneuver capableUnknown
ADEOS 2Payload
NORAD 27597
CountryJPN
Launched2002-12-14
COSPAR2002-056A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 802 KMISS 420Starlink 550

At 802 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 · YAOGAN-40 04A ⟷ ADEOS 2
2026-11-13 08:381.66 km Live forecast13.51 km/s802 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
12 Nov 11:47 UTC1.66 km Forecast13 Nov 08:38 UTC12 Nov 04:30 UTCRe-check
12 Nov 11:28 UTC5.66 km Forecast13 Nov 08:38 UTC12 Nov 04:30 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.41 km11-13 08:39 UTC
YAOGAN-40 04AIRIDIUM 33 DEB
1.69 km11-07 02:58 UTC
YAOGAN-40 04AIRIDIUM 149
1.71 km11-10 16:50 UTC
YAOGAN-40 04AOPS 1294 (DMSP 5D-2 F7)

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 →