HomeManeuver TrackerClose ApproachesMETEOR 2-6 ⟷ CZ-4B DEB
high · CROSS-BORDER
6.87 kmmiss distance
Closest approach (TCA)
2026-09-14 22:59 UTC
Relative speed
7.20 km/s
Altitude
Current separation
Share 𝕏 R

On 2026-09-14 22:59 UTC, RU METEOR 2-6 and CN CZ-4B DEB reached a closest approach (TCA) of 6.87 km, with a relative velocity of 7.20 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
METEOR 2-6Payload
NORAD 11962
CountryCIS
Launched1980-09-09
COSPAR1980-073A
Maneuver capableUnknown
CZ-4B DEBDebris
NORAD 27433
CountryPRC
Launched2002-05-15
COSPAR2002-024D
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 · 844 KMISS 420Starlink 550

At 844 km this pass sits inside the most congested band in low Earth orbit, home to the debris left by the 2007 ASAT test and the 2009 collision. 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 recorded passes under 10 km
Pair history · METEOR 2-6 ⟷ CZ-4B DEB
Now6.87 km7.20 km/s844 kmThis page
Now8.35 km14.77 km/s829 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
5.90 km09-15 12:45 UTC
METEOR 2-6SL-16 DEB
7.30 km09-09 13:42 UTC
METEOR 2-6SL-16 DEB
9.24 km09-14 04:12 UTC
METEOR 2-6ARGOS

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 — “METEOR 2-6 ⟷ CZ-4B DEB: 6.87 km close approach”, https://orbitalradar.com/conjunction/11962-27433 (accessed 2026-09-15).