Home›Maneuver Tracker›Close Approaches›YAOGAN-33 02 ⟷ SENTINEL-1D
MediumProximity
Final forecastFinal forecast, made minutes before the pass.
After the passBest estimate, from the orbit data published nearest its time: 7.88 km at 23 Oct 06:36 UTC.
Closest approach23 Oct 202606:36 UTC
Drift speed55 m/s199 km/h, seen from SENTINEL-1D
Altitude688 kmlow Earth orbit
Last confirmed23 Oct06:36 UTC · final forecast

CN YAOGAN-33 02 and ESA SENTINEL-1D were predicted to reach a closest approach of 8.20 km at 2026-10-23 06:36 UTC, drifting past at about 55 m/s (199 km/h) as seen from SENTINEL-1D. Final forecast, made minutes before the pass. Best estimate after the pass, from the orbit data published nearest its time: 7.88 km at 23 Oct 06:36 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
NORAD 53698
CountryPRC
Launched2022-09-02
COSPAR2022-106A
Maneuver capableUnknown
NORAD 66315
CountryESA
Launched2025-11-04
COSPAR2025-251A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 688 KMISS 420Starlink 550

At 688 km this pass sits inside the most congested band in low Earth orbit, home to the debris left by the 2007 ASAT test and the 2009 collision. 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

3 predicted passes under 10 km
Pair history · YAOGAN-33 02 ⟷ SENTINEL-1D
2026-10-23 06:368.20 km Final forecast0.06 km/s688 kmShown above
2026-10-23 05:472.81 km Final forecast0.06 km/s705 kmView →
2026-10-23 04:585.13 km Final forecast0.06 km/s688 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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 10:59 UTC7.88 km Best estimate23 Oct 06:36 UTC23 Oct 04:33 UTCBest estimate
23 Oct 05:56 UTC8.20 km Forecast23 Oct 06:36 UTC22 Oct 17:02 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.71 km10-21 16:43 UTC
YAOGAN-33 02CZ-6A DEB
2.22 km10-27 14:53 UTC
YAOGAN-33 02FENGYUN 1C DEB
3.09 km10-24 16:20 UTC
YAOGAN-33 02KITSAT 3

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-33 02 ⟷ SENTINEL-1D: 8.20 km predicted close approach”, https://orbitalradar.com/conjunction/53698-66315 (accessed 2026-10-26).