HomeManeuver TrackerClose ApproachesSJ-26 ⟷ IRIDIUM 33 DEB
high · CROSS-BORDER
5.59 kmmiss distance
Closest approach (TCA)
2026-09-18 02:44 UTC
Relative speed
13.23 km/s
Altitude
Current separation
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On 2026-09-18 02:44 UTC, CN SJ-26 and US IRIDIUM 33 DEB reached a closest approach (TCA) of 5.59 km, with a relative velocity of 13.23 km/s. This is a cross-border encounter between objects of different nations, the kind of event closely watched for space-security implications. Miss distance and time of closest approach are computed by propagating the latest published orbital elements for both objects, and values update as new element sets are published. See the Satellite Maneuver Tracker for the live picture and space situational awareness for context.

Why it mattersOne side of this pass cannot maneuver, so any avoidance decision rests with the other operator. Screening continues as new element sets arrive.

The Two Objects

Dossiers from the satellite directory
SJ-26Payload
NORAD 64199
CountryPRC
Launched2025-05-29
COSPAR2025-115A
Maneuver capableUnknown
NORAD 35484
CountryUS
Launched1997-09-14
COSPAR1997-051QE
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 479 KMISS 420Starlink 550

At 479 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 recorded pass under 10 km
Pair history · SJ-26 ⟷ IRIDIUM 33 DEB
Now5.59 km13.23 km/s479 kmThis page

Repeat encounters are common for objects in near-intersecting orbital planes; each pass is re-screened as fresh element sets arrive.

These Objects Elsewhere

Other screened approaches · 7 days
3.94 km09-17 13:55 UTC
SJ-26STARLINK-30068
6.47 km09-17 18:22 UTC
SJ-26STARLINK-30753
7.38 km09-16 20:29 UTC
YAOGAN-36 05AIRIDIUM 33 DEB

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 — “SJ-26 ⟷ IRIDIUM 33 DEB: 5.59 km close approach”, https://orbitalradar.com/conjunction/35484-64199 (accessed 2026-09-17).