Home›Maneuver Tracker›Close Approaches›SHIYAN 32-03 ⟷ OBJECT E
HighProximity
Final forecastFinal forecast, made minutes before the pass.
Closest approach24 Oct 202617:49 UTC
Relative speed10.09 km/sat the closest approach
Altitude442 kmlow Earth orbit
Last confirmed24 Oct17:49 UTC · final forecast

CN SHIYAN 32-03 and TBD OBJECT E were predicted to reach a closest approach of 1.73 km at 2026-10-24 17:49 UTC, at a relative speed of 10.09 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 66379
CountryPRC
Launched2025-11-08
COSPAR2025-255D
Maneuver capableUnknown
OBJECT EPayload
NORAD 63214
CountryTBD
Launched2025-03-15
COSPAR2025-052E
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 442 KMISS 420Starlink 550

At 442 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 32-03 ⟷ OBJECT E
2026-10-24 17:491.73 km Final forecast10.09 km/s442 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
24 Oct 12:29 UTC1.73 km Forecast24 Oct 17:49 UTC24 Oct 06:36 UTCRe-check
24 Oct 00:29 UTC4.36 km Forecast24 Oct 17:49 UTC23 Oct 18:09 UTCRe-check
23 Oct 18:29 UTC3.32 km Forecast24 Oct 17:49 UTC23 Oct 05:42 UTCRe-check
23 Oct 18:09 UTC2.78 km Forecast24 Oct 17:49 UTC23 Oct 04:08 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.82 km10-24 08:44 UTC
SHIYAN 32-03RUNNER-1 (TYVAK-1005)
2.27 km10-23 02:56 UTC
SHIYAN 32-03A-SEANSAT-PG1
2.69 km10-21 19:53 UTC
SHIYAN 32-03STARLINK-1558

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 32-03 ⟷ OBJECT E: 1.73 km predicted close approach”, https://orbitalradar.com/conjunction/63214-66379 (accessed 2026-10-25).