Home›Maneuver Tracker›Close Approaches›YAOGAN 11 ⟷ GEESAT 1-01
HighProximity
Live forecastConfirmed by the latest screening, 23 Oct 09:17 UTC.
Closest approach23 Oct 202618:02 UTC
Relative speed14.38 km/sat the closest approach
Altitude603 kmlow Earth orbit
Separation now—live

CN YAOGAN 11 and CN GEESAT 1-01 are predicted to reach a closest approach of 4.16 km at 2026-10-23 18:02 UTC, at a relative speed of 14.38 km/s. Confirmed by the latest screening, 23 Oct 09:17 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
YAOGAN 11Payload
NORAD 37165
CountryPRC
Launched2010-09-22
COSPAR2010-047A
Maneuver capableUnknown
NORAD 52785
CountryPRC
Launched2022-06-02
COSPAR2022-058A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 603 KMISS 420Starlink 550

At 603 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 11 ⟷ GEESAT 1-01
2026-10-23 18:024.16 km Live forecast14.38 km/s603 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
22 Oct 22:16 UTC4.16 km Forecast23 Oct 18:02 UTC22 Oct 15:26 UTCRe-check
22 Oct 21:57 UTC4.11 km Forecast23 Oct 18:02 UTC22 Oct 06:16 UTCRe-check
22 Oct 21:42 UTC7.33 km Forecast23 Oct 18:02 UTC22 Oct 06:16 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.15 km10-23 12:12 UTC
YAOGAN 11COSMOS 2251 DEB
3.27 km10-20 15:32 UTC
YAOGAN 11PSLV DEB
5.32 km10-23 08:46 UTC
YAOGAN 11SHIYAN 23 (SY-23)

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 →

Cite this encounter: Orbital Radar — “YAOGAN 11 ⟷ GEESAT 1-01: 4.16 km predicted close approach”, https://orbitalradar.com/conjunction/37165-52785 (accessed 2026-10-23).