Home›Maneuver Tracker›Close Approaches›CAPELLA-21 (ACADIA) ⟷ PELICAN-12
HighProximity
Final forecastFinal forecast, made 7 min before the pass.
Closest approach10 Nov 202620:13 UTC
Drift speed3.9 m/s14 km/h, seen from PELICAN-12
Altitude589 kmlow Earth orbit
Last confirmed10 Nov20:06 UTC · final forecast

US CAPELLA-21 (ACADIA) and US PELICAN-12 were predicted to reach a closest approach of 2.10 km at 2026-11-10 20:13 UTC, drifting past at about 3.9 m/s (14 km/h) as seen from PELICAN-12. 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 101118
CountryUS
Launched2026-10-20
COSPAR2026-237H
Maneuver capableUnknown
PELICAN-12Payload
NORAD 101128
CountryUS
Launched2026-10-20
COSPAR2026-237T
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 589 KMISS 420Starlink 550

At 589 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 · CAPELLA-21 (ACADIA) ⟷ PELICAN-12
2026-11-10 21:429.71 km Final forecast0.01 km/s590 kmView →
2026-11-10 21:022.94 km Final forecast0.00 km/s584 kmView →
2026-11-10 20:132.10 km Final forecast0.00 km/s589 kmShown above
2026-11-10 19:05989 m Not re-confirmed0.00 km/s585 kmView →
2026-11-10 18:031.50 km Withdrawn0.00 km/s589 kmView →
2026-11-10 18:031.50 km Withdrawn0.00 km/s589 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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 14:28 UTC2.10 km Forecast10 Nov 20:13 UTC10 Nov 11:05 UTCRe-check
10 Nov 03:51 UTC1.82 km Forecast10 Nov 20:41 UTC10 Nov 00:26 UTCRe-check
9 Nov 21:51 UTC1.86 km Forecast10 Nov 20:17 UTC9 Nov 16:45 UTCRe-check
9 Nov 20:14 UTC1.68 km Forecast10 Nov 20:20 UTC9 Nov 15:56 UTCRe-check
9 Nov 19:54 UTC5.66 km Forecast10 Nov 19:54 UTC9 Nov 15:56 UTCScreen
9 Nov 19:34 UTC8.45 km Forecast10 Nov 19:34 UTC9 Nov 15:56 UTCScreen
9 Nov 19:14 UTC8.71 km Forecast10 Nov 19:07 UTC9 Nov 15:56 UTCScreen
9 Nov 18:54 UTC9.25 km Forecast10 Nov 18:54 UTC9 Nov 15:56 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
244 m11-09 18:50 UTC
PELICAN-12TURKSAT 3U
477 m11-07 19:02 UTC
CAPELLA-21 (ACADIA)ICEYE-X110
638 m11-06 20:25 UTC
PELICAN-12ICEYE-X109

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 →