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COSMOS 1375 DEB

NORAD 16381 Debris LEO 1982-055V
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
979 km
Apogee
1066 km
Inclination
65.8°
Period
105.6 min
Mean Motion
13.63674063 rev/day
TLE Epoch
2026-06-18 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,023 km
Orbital Velocity26,433 km/h
Velocity7.34 km/s
Orbital Period106 minutes
Orbits / Day13.64
Eccentricity0.0059
Semi-Major Axis7,394 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1982-06-06
Launch Site
PKMTR
Int'l Designator
1982-055V
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 1375 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1982-06-06 from PKMTR. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 979 km and 1,066 km with an inclination of 65.8°. It travels at approximately 26,433 km/h (7.34 km/s), completing one full orbit every 106 minutes — that’s roughly 13.64 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, COSMOS 1375 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 1375 DEB orbits at an average altitude of 1,023 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of COSMOS 1375 DEB’s average altitude, there are currently 279 active payloads and 688 tracked debris or rocket body fragments. With an inclination of 65.8°, COSMOS 1375 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, of which 125 share a similar altitude band with COSMOS 1375 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 1375 DEB orbits in Low Earth Orbit (LEO) at altitudes between 979 km (perigee) and 1,066 km (apogee), with an average altitude of approximately 1,023 km. It completes one orbit every 106 minutes, travelling at approximately 26,433 km/h (16,425 mph).
COSMOS 1375 DEB (NORAD ID 16381) 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 1375 DEB was launched on 1982-06-06 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 1375 DEB (NORAD ID 16381) 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 1375 DEB travels at approximately 26,433 km/h (16,425 mph) — roughly 7.34 km/s. It completes 13.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.34 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 1375 DEB. Read more about debris statistics and the Kessler syndrome.