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COSMOS 252 DEB *

NORAD 18648 Debris LEO 1968-097ED
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
702 km
Apogee
1530 km
Inclination
62.2°
Period
107.6 min
Mean Motion
13.38149345 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,116 km
Orbital Velocity26,267 km/h
Velocity7.30 km/s
Orbital Period108 minutes
Orbits / Day13.38
Eccentricity0.0553
Semi-Major Axis7,487 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1968-11-01
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1968-097ED
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, 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 702 km and 1,530 km with an inclination of 62.2°. It travels at approximately 26,267 km/h (7.30 km/s), completing one full orbit every 108 minutes — that’s roughly 13.38 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,116 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 277 active payloads and 364 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041, ONEWEB-0250. 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.
🔗 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 702 km (perigee) and 1,530 km (apogee), with an average altitude of approximately 1,116 km. It completes one orbit every 108 minutes, travelling at approximately 26,267 km/h (16,322 mph).
COSMOS 252 DEB * (NORAD ID 18648) 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 252 DEB * (NORAD ID 18648) 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 26,267 km/h (16,322 mph) — roughly 7.30 km/s. It completes 13.38 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 7.30 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.