HomeManeuver TrackerClose ApproachesCOSMOS 952 ⟷ IRS 1B
high · PROXIMITY
4.76 kmmiss distance
Closest approach (TCA)
2026-09-11 20:30 UTC
Relative speed
4.43 km/s
Altitude
Current separation
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On 2026-09-11 20:30 UTC, RU COSMOS 952 and IN IRS 1B reached a closest approach (TCA) of 4.76 km, with a relative velocity of 4.43 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 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
COSMOS 952Payload
NORAD 10358
CountryCIS
Launched1977-09-16
COSPAR1977-088A
Maneuver capableUnknown
IRS 1BPayload
NORAD 21688
CountryIND
Launched1991-08-29
COSPAR1991-061A
Maneuver capableUnknown

Where This Happens

Altitude context
DEBRIS BELT 700–1000 KM2006001,0001,5002,000 kmTHIS PASS · 917 KMISS 420Starlink 550

At 917 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 952 ⟷ IRS 1B
Now4.76 km4.43 km/s917 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
4.65 km09-13 18:30 UTC
COSMOS 1275 DEBIRS 1B
5.86 km09-09 09:22 UTC
COSMOS 952SL-16 DEB
6.40 km09-08 23:05 UTC
COSMOS 952COSMOS 1375 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 — “COSMOS 952 ⟷ IRS 1B: 4.76 km close approach”, https://orbitalradar.com/conjunction/10358-21688 (accessed 2026-09-15).