Home›Maneuver Tracker›Close Approaches›YAOGAN 10 ⟷ GEESAT 3-08
HighProximity
Final forecastFinal forecast, made 9 min before the pass.
Closest approach5 Nov 202610:02 UTC
Relative speed14.51 km/sat the closest approach
Altitude614 kmlow Earth orbit
Last confirmed5 Nov09:53 UTC · final forecast

CN YAOGAN 10 and CN GEESAT 3-08 were predicted to reach a closest approach of 1.25 km at 2026-11-05 10:02 UTC, at a relative speed of 14.51 km/s. Final forecast, made 9 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
YAOGAN 10Payload
NORAD 36834
CountryPRC
Launched2010-08-09
COSPAR2010-038A
Maneuver capableUnknown
NORAD 61018
CountryPRC
Launched2024-09-05
COSPAR2024-159H
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 614 KMISS 420Starlink 550

At 614 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 · YAOGAN 10 ⟷ GEESAT 3-08
2026-11-05 10:021.25 km Final forecast14.51 km/s614 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
5 Nov 09:11 UTC1.25 km Forecast5 Nov 10:02 UTC4 Nov 23:43 UTCRe-check
4 Nov 17:58 UTC1.64 km Forecast5 Nov 10:02 UTC4 Nov 12:55 UTCRe-check
4 Nov 12:52 UTC1.72 km Forecast5 Nov 10:02 UTC4 Nov 04:34 UTCRe-check
4 Nov 12:32 UTC6.57 km Forecast5 Nov 10:02 UTC4 Nov 04:34 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
862 m10-31 08:43 UTC
YAOGAN 10GEESAT 5-06
2.90 km10-31 14:03 UTC
YAOGAN 10CZ-6A DEB
3.32 km10-31 09:27 UTC
YAOGAN 10OSCAR 36 (UOSAT 12)

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 →