Home›Maneuver Tracker›Close Approaches›PTS-1 ⟷ ION SCV-012
HighProximity
Live forecastConfirmed by the latest screening, 6 Nov 21:14 UTC.
Closest approach6 Nov 202623:16 UTC
Relative speed13.73 km/sat the closest approach
Altitude590 kmlow Earth orbit
Separation now—live

US PTS-1 and IT ION SCV-012 are predicted to reach a closest approach of 1.60 km at 2026-11-06 23:16 UTC, at a relative speed of 13.73 km/s. Confirmed by the latest screening, 6 Nov 21:14 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
PTS-1Payload
NORAD 101137
CountryUS
Launched2026-10-20
COSPAR2026-237AC
Maneuver capableUnknown
NORAD 60573
CountryIT
Launched2024-08-16
COSPAR2024-149DK
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 590 KMISS 420Starlink 550

At 590 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 · PTS-1 ⟷ ION SCV-012
2026-11-06 23:161.60 km Live forecast13.73 km/s590 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 Nothing is overwritten: a withdrawn forecast keeps its figure, with the newer check beside it, and the best estimate after the pass is a row of its own.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
6 Nov 10:40 UTC1.60 km Forecast6 Nov 23:16 UTC5 Nov 21:51 UTCRe-check
6 Nov 10:20 UTC7.66 km Forecast6 Nov 23:16 UTC5 Nov 21:51 UTCScreen

These Objects Elsewhere

Other screened approaches · 7 days
84 m11-06 02:09 UTC
PTS-1ICEYE-X84
237 m11-05 23:48 UTC
PTS-1ICEYE-X84
783 m11-07 05:19 UTC
PTS-1BLACK KITE-2

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 →