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COSMOS 886 DEB

NORAD 9961 Debris LEO 1976-126BB
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
526 km
Apogee
1302 km
Inclination
65.8°
Period
103.3 min
Mean Motion
13.94160259 rev/day
TLE Epoch
2026-09-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude914 km
Orbital Velocity26,629 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.94
Eccentricity0.0533
Semi-Major Axis7,285 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-12-27
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1976-126BB
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 886 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1976-12-27 from Baikonur Cosmodrome, Kazakhstan on the IS launch. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 526 km and 1,302 km with an inclination of 65.8°. It travels at approximately 26,629 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.94 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, COSMOS 886 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
COSMOS 886 DEB orbits at an average altitude of 914 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of COSMOS 886 DEB’s average altitude, there are currently 290 active payloads and 1,413 tracked debris or rocket body fragments. With an inclination of 65.8°, COSMOS 886 DEB passes over latitudes between 65.8°N and 65.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,535 active satellites in total, of which 65 share a similar altitude band with COSMOS 886 DEB.
🔗 Tracked Space Debris

This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.

❓ Frequently Asked Questions
COSMOS 886 DEB orbits in Low Earth Orbit (LEO) at altitudes between 526 km (perigee) and 1,302 km (apogee), with an average altitude of approximately 914 km. It completes one orbit every 103 minutes, travelling at approximately 26,629 km/h (16,547 mph).
COSMOS 886 DEB (NORAD ID 9961) is a piece of tracked orbital debris attributed to Russia (CIS). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
COSMOS 886 DEB was launched on 1976-12-27 from Baikonur Cosmodrome, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 886 DEB (NORAD ID 9961) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
COSMOS 886 DEB travels at approximately 26,629 km/h (16,547 mph) — roughly 7.40 km/s. It completes 13.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.40 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like COSMOS 886 DEB. Read more about debris statistics and the Kessler syndrome.