HomeManeuver TrackerClose ApproachesCOSMOS 397 DEB * ⟷ COSMOS 2016
medium · PROXIMITY
6.45 kmmiss distance
Closest approach (TCA)
2026-09-15 16:03 UTC
Relative speed
4.38 km/s
Altitude
Current separation
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On 2026-09-15 16:03 UTC, RU COSMOS 397 DEB * and RU COSMOS 2016 reached a closest approach (TCA) of 6.45 km, with a relative velocity of 4.38 km/s. 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
NORAD 14446
CountryCIS
Launched1971-02-25
COSPAR1971-015CQ
Maneuver capableNo
Uncontrolled debris fragment tracked by the public catalogue. About space debris →
NORAD 19921
CountryCIS
Launched1989-04-04
COSPAR1989-028A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 984 KMISS 420Starlink 550

At 984 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

1 recorded pass under 10 km
Pair history · COSMOS 397 DEB * ⟷ COSMOS 2016
Now6.45 km4.38 km/s984 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
2.31 km09-11 13:36 UTC
COSMOS 397 DEB *SL-16 DEB
3.48 km09-09 11:48 UTC
COSMOS 1808COSMOS 2016
5.79 km09-09 22:15 UTC
COSMOS 1275 DEBCOSMOS 2016

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 — “COSMOS 397 DEB * ⟷ COSMOS 2016: 6.45 km close approach”, https://orbitalradar.com/conjunction/14446-19921 (accessed 2026-09-15).