Home›Maneuver Tracker›Close Approaches›PELICAN-12 ⟷ ICEYE-X109
CriticalProximity
Final forecastFinal forecast, made 14 min before the pass.
After the passBest estimate, from the orbit data published nearest its time: within 40 minutes of the predicted time the two stayed at least 2.51 km apart.
Closest approach6 Nov 202620:25 UTC
Drift speed0.8 m/s3 km/h, seen from ICEYE-X109
Altitude586 kmlow Earth orbit
Last confirmed6 Nov20:11 UTC · final forecast

US PELICAN-12 and NETH ICEYE-X109 were predicted to reach a closest approach of 638 m at 2026-11-06 20:25 UTC, drifting past at about 0.8 m/s (3 km/h) as seen from ICEYE-X109. Final forecast, made 14 min before the pass. Best estimate after the pass, from the orbit data published nearest its time: within 40 minutes of the predicted time the two stayed at least 2.51 km apart. 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
PELICAN-12Payload
NORAD 101128
CountryUS
Launched2026-10-20
COSPAR2026-237T
Maneuver capableUnknown
ICEYE-X109Payload
NORAD 101124
CountryNETH
Launched2026-10-20
COSPAR2026-237P
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 586 KMISS 420Starlink 550

At 586 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

6 predicted passes under 10 km
Pair history · PELICAN-12 ⟷ ICEYE-X109
2026-11-06 22:547.90 km Final forecast · after: ≥986 m0.01 km/s591 kmView →
2026-11-06 20:25638 m Final forecast · after: ≥2.51 km0.00 km/s586 kmShown above
2026-11-06 18:151.50 km Withdrawn · after: ≥12.8 km0.00 km/s589 kmView →
2026-11-06 17:341.40 km Withdrawn · after: ≥14.8 km0.00 km/s587 kmView →
2026-11-06 16:521.30 km Withdrawn · after: ≥20.3 km0.00 km/s588 kmView →
2026-11-06 14:431.78 km Withdrawn · after: ≥28.7 km0.00 km/s591 kmView →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
10 Nov 18:46 UTC2.51 km Best estimate6 Nov 21:05 UTC6 Nov 20:14 UTCBest estimate
6 Nov 18:50 UTC638 m Forecast6 Nov 20:25 UTC6 Nov 14:47 UTCRe-check
6 Nov 12:50 UTC392 m Forecast6 Nov 20:26 UTC6 Nov 08:45 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
244 m11-09 18:50 UTC
PELICAN-12TURKSAT 3U
989 m11-10 19:05 UTC
CAPELLA-21 (ACADIA)PELICAN-12
1.16 km11-10 04:31 UTC
PELICAN-12ICEYE-X110

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 →