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COSMOS 1823 DEB

NORAD 18728 Debris LEO 1987-020F
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1470 km
Apogee
1577 km
Inclination
73.6°
Period
116.5 min
Mean Motion
12.36057995 rev/day
TLE Epoch
2026-06-25 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,524 km
Orbital Velocity25,581 km/h
Velocity7.11 km/s
Orbital Period117 minutes
Orbits / Day12.36
Eccentricity0.0068
Semi-Major Axis7,895 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1987-02-20
Launch Site
PKMTR
Int'l Designator
1987-020F
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 on the Musson No. 19 launch. With over 39 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,470 km and 1,577 km with an inclination of 73.6°. It travels at approximately 25,581 km/h (7.11 km/s), completing one full orbit every 117 minutes — that’s roughly 12.36 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 1,524 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 167 active payloads and 261 tracked debris or rocket body fragments. With an inclination of 73.6°, COSMOS 1823 DEB passes over latitudes between 73.6°N and 73.6°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 156 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 1,470 km (perigee) and 1,577 km (apogee), with an average altitude of approximately 1,524 km. It completes one orbit every 117 minutes, travelling at approximately 25,581 km/h (15,895 mph).
COSMOS 1823 DEB (NORAD ID 18728) 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 18728) 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 25,581 km/h (15,895 mph) — roughly 7.11 km/s. It completes 12.36 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 7.11 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.