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COSMOS 839 DEB *

NORAD 21957 Debris LEO 1976-067BV
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
833 km
Apogee
1966 km
Inclination
65.5°
Period
113.8 min
Mean Motion
12.65741451 rev/day
TLE Epoch
2026-06-18 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,400 km
Orbital Velocity25,784 km/h
Velocity7.16 km/s
Orbital Period114 minutes
Orbits / Day12.66
Eccentricity0.0729
Semi-Major Axis7,771 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1976-07-08
Launch Site
PKMTR
Int'l Designator
1976-067BV
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 839 DEB * is a tracked piece of space debris attributed to Russia (CIS), launched on 1976-07-08 from PKMTR. 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 833 km and 1,966 km with an inclination of 65.5°. It travels at approximately 25,784 km/h (7.16 km/s), completing one full orbit every 114 minutes — that’s roughly 12.66 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, COSMOS 839 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 839 DEB * orbits at an average altitude of 1,400 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 839 DEB *’s average altitude, there are currently 242 active payloads and 162 tracked debris or rocket body fragments. With an inclination of 65.5°, COSMOS 839 DEB * passes over latitudes between 65.5°N and 65.5°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 208 share a similar altitude band with COSMOS 839 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 839 DEB * orbits in Low Earth Orbit (LEO) at altitudes between 833 km (perigee) and 1,966 km (apogee), with an average altitude of approximately 1,400 km. It completes one orbit every 114 minutes, travelling at approximately 25,784 km/h (16,021 mph).
COSMOS 839 DEB * (NORAD ID 21957) 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 839 DEB * was launched on 1976-07-08 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 839 DEB * (NORAD ID 21957) 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 839 DEB * travels at approximately 25,784 km/h (16,021 mph) — roughly 7.16 km/s. It completes 12.66 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 7.16 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 839 DEB *. Read more about debris statistics and the Kessler syndrome.