Home›Maneuver Tracker›Close Approaches›SHIYAN 30 02 ⟷ ICEYE-X75
HighProximity
Final forecastFinal forecast, made minutes before the pass.
Closest approach26 Oct 202620:04 UTC
Relative speed9.88 km/sat the closest approach
Altitude594 kmlow Earth orbit
Last confirmed26 Oct20:04 UTC · final forecast

CN SHIYAN 30 02 and POL ICEYE-X75 were predicted to reach a closest approach of 4.29 km at 2026-10-26 20:04 UTC, at a relative speed of 9.88 km/s. Final forecast, made minutes 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
NORAD 65852
CountryPRC
Launched2025-09-29
COSPAR2025-222B
Maneuver capableUnknown
ICEYE-X75Payload
NORAD 68497
CountryPOL
Launched2026-03-30
COSPAR2026-067CK
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 594 KMISS 420Starlink 550

At 594 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 · SHIYAN 30 02 ⟷ ICEYE-X75
2026-10-26 20:044.29 km Final forecast9.88 km/s594 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
26 Oct 16:41 UTC4.29 km Forecast26 Oct 20:04 UTC26 Oct 04:32 UTCRe-check
26 Oct 10:28 UTC4.26 km Forecast26 Oct 20:04 UTC25 Oct 23:43 UTCRe-check
26 Oct 10:06 UTC4.43 km Forecast26 Oct 20:04 UTC25 Oct 23:43 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
2.59 km10-23 19:27 UTC
SHIYAN 30 02MARINA
3.20 km10-28 16:10 UTC
SHIYAN 30 02OBJECT C
3.42 km10-29 01:16 UTC
SHIYAN 30 02COSMOS 2535 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 →

Cite this encounter: Orbital Radar — “SHIYAN 30 02 ⟷ ICEYE-X75: 4.29 km predicted close approach”, https://orbitalradar.com/conjunction/65852-68497 (accessed 2026-10-29).