Home›Maneuver Tracker›Close Approaches›SHIYAN 30 01 ⟷ SATORO-T3
HighProximity
ChinaSHIYAN 30 01NORAD 65851 · launched Sep 2025Military payload
1.90kmPredicted miss distance
SINGSATORO-T3NORAD 64589 · launched Jun 2025Payload
Final forecastFinal forecast, made 17 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: 2.09 km at 8 Nov 00:38 UTC.
Closest approach8 Nov 202600:38 UTC
Relative speed9.45 km/sat the closest approach
Altitude591 kmlow Earth orbit
Last confirmed8 Nov00:21 UTC · final forecast
Track SHIYAN 30 01Track SATORO-T3All approaches
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CN SHIYAN 30 01 and SING SATORO-T3 were predicted to reach a closest approach of 1.90 km at 2026-11-08 00:38 UTC, at a relative speed of 9.45 km/s. Final forecast, made 17 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: 2.09 km at 8 Nov 00:38 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
SHIYAN 30 01Payload
NORAD 65851
CountryPRC
Launched2025-09-29
OrbitLEO · 589 × 593 km
COSPAR2025-222A
Maneuver capableUnknown
Profile →Globe →
SATORO-T3Payload
NORAD 64589
CountrySING
Launched2025-06-23
OrbitLEO · 579 × 586 km
COSPAR2025-135BP
Maneuver capableUnknown
Profile →Globe →

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 591 KMISS 420Starlink 550

At 591 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

2 predicted passes under 10 km
Pair history · SHIYAN 30 01 ⟷ SATORO-T3
2026-11-08 00:381.90 km Final forecast · after: 2.09 km9.45 km/s591 kmShown above
2026-11-07 23:508.97 km Final forecast · after: 9.00 km9.47 km/s584 kmView →

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 13:27 UTC2.09 km Best estimate8 Nov 00:38 UTC7 Nov 21:41 UTCBest estimate
7 Nov 12:51 UTC1.90 km Forecast8 Nov 00:38 UTC7 Nov 07:06 UTCRe-check
7 Nov 12:32 UTC8.92 km Forecast8 Nov 00:38 UTC6 Nov 21:35 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
461 m11-07 10:48 UTC
SHIYAN 30 01KITA-36
616 m11-09 12:00 UTC
SHIYAN 30 02SATORO-T3
1.76 km11-10 04:53 UTC
SHIYAN 30 01IRIDE-MS2-HEO-6

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 →