COSMOS 252 DEB
NORAD 18556
Debris
LEO
1968-097EP
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LEO · NORAD 18556
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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
668 km
Apogee
1247 km
Inclination
62.2°
Period
104.2 min
Mean Motion
13.81742234 rev/day
TLE Epoch
2026-06-19 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude958 km
Orbital Velocity26,550 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.82
Eccentricity0.0395
Semi-Major Axis7,329 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1968-11-01
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1968-097EP
Object Type
Debris
RCS Size
Small (<0.1 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, Kazakhstan. 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 668 km and 1,247 km with an inclination of 62.2°. It travels at approximately 26,550 km/h (7.37 km/s), completing one full orbit every 104 minutes — that’s roughly 13.82 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 958 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 252 DEB’s average altitude, there are currently 299 active payloads and 1,060 tracked debris or rocket body fragments. With an inclination of 62.2°, COSMOS 252 DEB passes over latitudes between 62.2°N and 62.2°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 164 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 668 km (perigee) and 1,247 km (apogee), with an average altitude of approximately 958 km. It completes one orbit every 104 minutes, travelling at approximately 26,550 km/h (16,497 mph).
COSMOS 252 DEB (NORAD ID 18556) 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, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 252 DEB (NORAD ID 18556) 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 26,550 km/h (16,497 mph) — roughly 7.37 km/s. It completes 13.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.37 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.