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COSMOS 886 DEB

NORAD 18518 Debris LEO 1976-126BW
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
786 km
Apogee
1884 km
Inclination
65.8°
Period
112.3 min
Mean Motion
12.81722451 rev/day
TLE Epoch
2026-06-25 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,335 km
Orbital Velocity25,891 km/h
Velocity7.19 km/s
Orbital Period112 minutes
Orbits / Day12.82
Eccentricity0.0712
Semi-Major Axis7,706 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1976-126BW
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, 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 786 km and 1,884 km with an inclination of 65.8°. It travels at approximately 25,891 km/h (7.19 km/s), completing one full orbit every 112 minutes — that’s roughly 12.82 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,335 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of COSMOS 886 DEB’s average altitude, there are currently 13 active payloads and 161 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. 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 1,286 active satellites in total.
🔗 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 786 km (perigee) and 1,884 km (apogee), with an average altitude of approximately 1,335 km. It completes one orbit every 112 minutes, travelling at approximately 25,891 km/h (16,088 mph).
COSMOS 886 DEB (NORAD ID 18518) 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, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 886 DEB (NORAD ID 18518) 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 25,891 km/h (16,088 mph) — roughly 7.19 km/s. It completes 12.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.19 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.