COSMOS 886 DEB
NORAD 19244
Debris
LEO
1976-126CA
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LEO · NORAD 19244
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
868 km
Apogee
1997 km
Inclination
66.0°
Period
114.5 min
Mean Motion
12.57638879 rev/day
TLE Epoch
2026-06-15 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,433 km
Orbital Velocity25,729 km/h
Velocity7.15 km/s
Orbital Period115 minutes
Orbits / Day12.58
Eccentricity0.0723
Semi-Major Axis7,804 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-12-27
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1976-126CA
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 Low Earth Orbit (LEO) at altitudes between 868 km and 1,997 km with an inclination of 66.0°. It travels at approximately 25,729 km/h (7.15 km/s), completing one full orbit every 115 minutes — that’s roughly 12.58 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 1,433 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 348 active payloads and 174 tracked debris or rocket body fragments. With an inclination of 66.0°, COSMOS 886 DEB passes over latitudes between 66.0°N and 66.0°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, of which 313 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 868 km (perigee) and 1,997 km (apogee), with an average altitude of approximately 1,433 km. It completes one orbit every 115 minutes, travelling at approximately 25,729 km/h (15,987 mph).
COSMOS 886 DEB (NORAD ID 19244) 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 19244) 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 25,729 km/h (15,987 mph) — roughly 7.15 km/s. It completes 12.58 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 7.15 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.