Home›Maneuver Tracker›Close Approaches›ICEYE-X37 ⟷ STRIX-10
HighProximity
Final forecastFinal forecast, made 6 min before the pass.
Closest approach5 Nov 202606:57 UTC
Relative speed8.88 km/sat the closest approach
Altitude543 kmlow Earth orbit
Last confirmed5 Nov06:51 UTC · final forecast

US ICEYE-X37 and JP STRIX-10 were predicted to reach a closest approach of 1.90 km at 2026-11-05 06:57 UTC, at a relative speed of 8.88 km/s. Final forecast, made 6 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
ICEYE-X37Payload
NORAD 59102
CountryUS
Launched2024-03-04
COSPAR2024-043E
Maneuver capableUnknown
STRIX-10Payload
NORAD 100746
CountryJPN
Launched2026-09-19
COSPAR2026-217A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 543 KMISS 420Starlink 550

At 543 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 · ICEYE-X37 ⟷ STRIX-10
2026-11-05 06:571.90 km Final forecast8.88 km/s543 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.

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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
4 Nov 20:23 UTC1.90 km Forecast5 Nov 06:57 UTC4 Nov 09:19 UTCRe-check
4 Nov 20:03 UTC3.76 km Forecast5 Nov 06:57 UTC4 Nov 09:19 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
3.17 km11-03 00:32 UTC
ICEYE-X37PEGASUS R/B
3.94 km11-07 07:51 UTC
ICEYE-X37OBJECT E
4.86 km11-07 04:01 UTC
ICEYE-X37STARLINK-5970

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 →