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COSMOS 886 DEB

NORAD 14800 Debris MEO 1976-126BS
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1401 km
Apogee
2415 km
Inclination
65.8°
Period
125.1 min
Mean Motion
11.50916899 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,908 km
Orbital Velocity24,979 km/h
Velocity6.94 km/s
Orbital Period2 hours 5 minutes
Orbits / Day11.51
Eccentricity0.0612
Semi-Major Axis8,279 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1976-126BS
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 1,401 km and 2,415 km with an inclination of 65.8°. It travels at approximately 24,979 km/h (6.94 km/s), completing one full orbit every 2 hours 5 minutes — that’s roughly 11.51 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 1,908 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 5 active payloads and 17 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 1,285 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 Medium Earth Orbit (MEO) at altitudes between 1,401 km (perigee) and 2,415 km (apogee), with an average altitude of approximately 1,908 km. It completes one orbit every 2 hours 5 minutes, travelling at approximately 24,979 km/h (15,521 mph).
COSMOS 886 DEB (NORAD ID 14800) 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 14800) 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 24,979 km/h (15,521 mph) — roughly 6.94 km/s. It completes 11.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 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 6.94 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.