COSMOS 252 DEB
NORAD 3814
Debris
LEO
1968-097BC
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LEO · NORAD 3814
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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
743 km
Apogee
1943 km
Inclination
62.3°
Period
112.5 min
Mean Motion
12.79526983 rev/day
TLE Epoch
2026-09-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,343 km
Orbital Velocity25,878 km/h
Velocity7.19 km/s
Orbital Period113 minutes
Orbits / Day12.80
Eccentricity0.0778
Semi-Major Axis7,714 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1968-11-01
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1968-097BC
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 252 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1968-11-01 from Baikonur Cosmodrome, Kazakhstan on the I2P launch. After more than 58 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 743 km and 1,943 km with an inclination of 62.3°. It travels at approximately 25,878 km/h (7.19 km/s), completing one full orbit every 113 minutes — that’s roughly 12.80 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, COSMOS 252 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 252 DEB orbits at an average altitude of 1,343 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 252 DEB’s average altitude, there are currently 30 active payloads and 232 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 62.3°, COSMOS 252 DEB passes over latitudes between 62.3°N and 62.3°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 1,535 active satellites in total, of which 10 share a similar altitude band with COSMOS 252 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 252 DEB orbits in Low Earth Orbit (LEO) at altitudes between 743 km (perigee) and 1,943 km (apogee), with an average altitude of approximately 1,343 km. It completes one orbit every 113 minutes, travelling at approximately 25,878 km/h (16,080 mph).
COSMOS 252 DEB (NORAD ID 3814) 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 252 DEB was launched on 1968-11-01 from Baikonur Cosmodrome, 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 252 DEB (NORAD ID 3814) 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 252 DEB travels at approximately 25,878 km/h (16,080 mph) — roughly 7.19 km/s. It completes 12.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.19 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 252 DEB. Read more about debris statistics and the Kessler syndrome.