Home›Maneuver Tracker›Close Approaches›YAOGAN-30 J ⟷ EINSTEIN PROBE
HighProximity
Final forecastFinal forecast, made 7 min before the pass.
Closest approach14 Nov 202615:40 UTC
Drift speed800 m/s2,879 km/h, seen from EINSTEIN PROBE
Altitude552 kmlow Earth orbit
Last confirmed14 Nov15:33 UTC · final forecast

CN YAOGAN-30 J and CN EINSTEIN PROBE were predicted to reach a closest approach of 2.83 km at 2026-11-14 15:40 UTC, drifting past at about 800 m/s (2,879 km/h) as seen from EINSTEIN PROBE. Final forecast, made 7 min 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 43083
CountryPRC
Launched2017-12-25
COSPAR2017-085C
Maneuver capableUnknown
NORAD 58753
CountryPRC
Launched2024-01-09
COSPAR2024-007A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 552 KMISS 420Starlink 550

At 552 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

3 predicted passes under 10 km
Pair history · YAOGAN-30 J ⟷ EINSTEIN PROBE
2026-11-14 15:402.83 km Final forecast0.80 km/s552 kmShown above
2026-11-14 14:525.11 km Final forecast0.80 km/s561 kmView →
2026-11-14 14:058.71 km Final forecast0.80 km/s552 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
14 Nov 11:53 UTC2.83 km Forecast14 Nov 15:40 UTC14 Nov 07:44 UTCRe-check
14 Nov 09:02 UTC2.70 km Forecast14 Nov 15:40 UTC13 Nov 23:46 UTCRe-check
14 Nov 03:02 UTC2.88 km Forecast14 Nov 15:40 UTC13 Nov 11:00 UTCRe-check
13 Nov 16:04 UTC2.71 km Forecast14 Nov 15:40 UTC13 Nov 07:49 UTCRe-check
13 Nov 15:44 UTC2.81 km Forecast14 Nov 15:40 UTC13 Nov 07:49 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
1.88 km11-14 17:41 UTC
YAOGAN-30 JHBTSS-SV1
1.97 km11-12 05:44 UTC
YAOGAN-30 JSTARLINK-5848
4.17 km11-11 18:43 UTC
YAOGAN-30 JSTARLINK-6037

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 →