Home›Maneuver Tracker›Close Approaches›ELEMENT-1 ⟷ ICEYE-X86
MediumProximity
Live forecastConfirmed by the latest screening, 26 Oct 23:05 UTC.
Closest approach27 Oct 202612:49 UTC
Drift speed0.7 m/s3 km/h, seen from ICEYE-X86
Altitude508 kmlow Earth orbit
Separation now—live

US ELEMENT-1 and SWED ICEYE-X86 are predicted to reach a closest approach of 5.28 km at 2026-10-27 12:49 UTC, drifting past at about 0.7 m/s (3 km/h) as seen from ICEYE-X86. Confirmed by the latest screening, 26 Oct 23:05 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
ELEMENT-1Payload
NORAD 100901
CountryUS
Launched2026-10-01
COSPAR2026-227U
Maneuver capableUnknown
ICEYE-X86Payload
NORAD 100910
CountrySWED
Launched2026-10-01
COSPAR2026-227AD
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 508 KMISS 420Starlink 550

At 508 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 · ELEMENT-1 ⟷ ICEYE-X86
2026-10-27 14:26680 m Live forecast0.00 km/s506 kmView →
2026-10-27 12:495.28 km Live forecast0.01 km/s508 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
26 Oct 16:41 UTC5.28 km Forecast27 Oct 12:49 UTC26 Oct 03:26 UTCRe-check
26 Oct 12:47 UTC5.32 km Forecast27 Oct 12:49 UTC25 Oct 22:41 UTCRe-check
26 Oct 12:27 UTC6.62 km Forecast27 Oct 12:27 UTC25 Oct 22:41 UTCScreen
26 Oct 12:07 UTC9.14 km Forecast27 Oct 12:07 UTC25 Oct 22:41 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
75 m10-23 18:53 UTC
ELEMENT-1OBJECT AK
675 m10-23 20:00 UTC
ELEMENT-1OBJECT BS
851 m10-23 21:07 UTC
ELEMENT-1OBJECT BS

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 — “ELEMENT-1 ⟷ ICEYE-X86: 5.28 km predicted close approach”, https://orbitalradar.com/conjunction/100901-100910 (accessed 2026-10-26).