Home›Maneuver Tracker›Close Approaches›COSMOS 2538 ⟷ AE5RB
high · PROXIMITY
2.10 kmpredicted miss distance
Final forecastFinal forecast, made minutes before the pass.
Predicted closest approach
2026-10-20 09:23 UTC
Relative speed
1.03 km/s
Altitude
Last confirmed
20 Oct 09:18 UTC
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RU COSMOS 2538 and JP AE5RB were predicted to reach a closest approach of 2.10 km at 2026-10-20 09:23 UTC, at a relative speed of 1.03 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 44424
CountryCIS
Launched2019-07-10
COSPAR2019-039D
Maneuver capableUnknown
AE5RBPayload
NORAD 66693
CountryJPN
Launched2025-11-28
COSPAR2025-276AD
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 494 KMISS 420Starlink 550

At 494 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 · COSMOS 2538 ⟷ AE5RB
2026-10-20 09:232.10 km Final forecast1.03 km/s494 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.

These Objects Elsewhere

Other screened approaches · 7 days
1.54 km10-20 19:18 UTC
COSMOS 2538STARLINK-36125
1.95 km10-21 00:06 UTC
COSMOS 2538AEROCUBE 18B
3.39 km10-18 17:08 UTC
ICEYE-X83COSMOS 2538

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 — “COSMOS 2538 ⟷ AE5RB: 2.10 km predicted close approach”, https://orbitalradar.com/conjunction/44424-66693 (accessed 2026-10-21).