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COSMOS 886 DEB

NORAD 14503 Debris MEO 1976-126BQ
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
743 km
Apogee
2336 km
Inclination
65.9°
Period
116.9 min
Mean Motion
12.32236438 rev/day
TLE Epoch
2026-06-16 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,540 km
Orbital Velocity25,555 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.32
Eccentricity0.1007
Semi-Major Axis7,911 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1976-126BQ
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. After more than 50 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 743 km and 2,336 km with an inclination of 65.9°. It travels at approximately 25,555 km/h (7.10 km/s), completing one full orbit every 117 minutes — that’s roughly 12.32 orbits per day. Its orbital eccentricity of 0.1007 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 1,540 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of COSMOS 886 DEB’s average altitude, there are currently 119 active payloads and 260 tracked debris or rocket body fragments. With an inclination of 65.9°, COSMOS 886 DEB passes over latitudes between 65.9°N and 65.9°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 1,285 active satellites in total, of which 107 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 Medium Earth Orbit (MEO) at altitudes between 743 km (perigee) and 2,336 km (apogee), with an average altitude of approximately 1,540 km. It completes one orbit every 117 minutes, travelling at approximately 25,555 km/h (15,879 mph).
COSMOS 886 DEB (NORAD ID 14503) 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 14503) 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 25,555 km/h (15,879 mph) — roughly 7.10 km/s. It completes 12.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.10 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.