COSMOS 1823 DEB
NORAD 39822
Debris
LEO
1987-020EW
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LEO · NORAD 39822
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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
1446 km
Apogee
1649 km
Inclination
74.0°
Period
117.0 min
Mean Motion
12.30456901 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,548 km
Orbital Velocity25,542 km/h
Velocity7.09 km/s
Orbital Period117 minutes
Orbits / Day12.30
Eccentricity0.0128
Semi-Major Axis7,919 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1987-02-20
Launch Site
PKMTR
Int'l Designator
1987-020EW
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 1823 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1987-02-20 from PKMTR. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,446 km and 1,649 km with an inclination of 74.0°. It travels at approximately 25,542 km/h (7.09 km/s), completing one full orbit every 117 minutes — that’s roughly 12.30 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, COSMOS 1823 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 1823 DEB orbits at an average altitude of 1,548 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 1823 DEB’s average altitude, there are currently 52 active payloads and 252 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 74.0°, COSMOS 1823 DEB passes over latitudes between 74.0°N and 74.0°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 39 share a similar altitude band with COSMOS 1823 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 1823 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,446 km (perigee) and 1,649 km (apogee), with an average altitude of approximately 1,548 km. It completes one orbit every 117 minutes, travelling at approximately 25,542 km/h (15,871 mph).
COSMOS 1823 DEB (NORAD ID 39822) 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 1823 DEB was launched on 1987-02-20 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 1823 DEB (NORAD ID 39822) 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 1823 DEB travels at approximately 25,542 km/h (15,871 mph) — roughly 7.09 km/s. It completes 12.30 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 7.09 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 1823 DEB. Read more about debris statistics and the Kessler syndrome.