Home›Maneuver Tracker›Close Approaches›YAOGAN-39 02A ⟷ HADES-SA (SPINNYONE)
HighProximity
WithdrawnNewer orbit data from 24 Oct 22:12 UTC no longer shows this pass. Within 40 minutes of the predicted time the two stayed at least 75.6 km apart. The most recent pass the screening confirmed up to its time: 6.11 km on 22 Oct 18:50 UTC.
Closest approach26 Oct 202604:45 UTC
Relative speed13.80 km/sat the closest approach
Altitude493 kmlow Earth orbit
Last confirmed25 Oct09:40 UTC · withdrawn

CN YAOGAN-39 02A and SPN HADES-SA (SPINNYONE) were predicted to reach a closest approach of 4.21 km at 2026-10-26 04:45 UTC, at a relative speed of 13.80 km/s. Withdrawn: newer orbit data from 24 Oct 22:12 UTC no longer shows this pass. Within 40 minutes of the predicted time the two stayed at least 75.6 km apart. The figure above is the forecast as it was published; the newer check is shown beside it, and nothing is overwritten. 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 57886
CountryPRC
Launched2023-09-17
COSPAR2023-145A
Maneuver capableUnknown
NORAD 68446
CountrySPN
Launched2026-03-30
COSPAR2026-067AG
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 493 KMISS 420Starlink 550

At 493 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 · YAOGAN-39 02A ⟷ HADES-SA (SPINNYONE)
2026-10-26 04:454.21 km Withdrawn13.80 km/s493 kmShown above
2026-10-22 18:506.11 km Final forecast13.23 km/s491 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
25 Oct 09:59 UTC75.63 km Withdrawn26 Oct 04:46 UTC24 Oct 22:12 UTCRe-check
25 Oct 09:10 UTC4.21 km Forecast26 Oct 04:45 UTC23 Oct 14:44 UTCRe-check
25 Oct 08:51 UTC5.43 km Forecast26 Oct 04:45 UTC23 Oct 14:44 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
3.39 km10-26 14:59 UTC
YAOGAN-39 02ACOSMOS 2573
5.15 km10-24 03:30 UTC
YAOGAN-39 02AKSM1-B
5.80 km10-19 19:28 UTC
YAOGAN-39 02AOBJECT D

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-39 02A ⟷ HADES-SA (SPINNYONE): 4.21 km forecast, withdrawn”, https://orbitalradar.com/conjunction/57886-68446 (accessed 2026-10-26).