COSMOS 252 DEB *
NORAD 3938
Debris
MEO
1968-097BS
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MEO · NORAD 3938
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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
603 km
Apogee
2272 km
Inclination
63.0°
Period
114.6 min
Mean Motion
12.56448822 rev/day
TLE Epoch
2026-09-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,438 km
Orbital Velocity25,721 km/h
Velocity7.14 km/s
Orbital Period115 minutes
Orbits / Day12.56
Eccentricity0.1069
Semi-Major Axis7,809 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
1968-097BS
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 Medium Earth Orbit (MEO) at altitudes between 603 km and 2,272 km with an inclination of 63.0°. It travels at approximately 25,721 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.56 orbits per day. Its orbital eccentricity of 0.1069 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 1,438 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of COSMOS 252 DEB *’s average altitude, there are currently 502 active payloads and 307 tracked debris or rocket body fragments. With an inclination of 63.0°, COSMOS 252 DEB * passes over latitudes between 63.0°N and 63.0°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 443 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 Medium Earth Orbit (MEO) at altitudes between 603 km (perigee) and 2,272 km (apogee), with an average altitude of approximately 1,438 km. It completes one orbit every 115 minutes, travelling at approximately 25,721 km/h (15,982 mph).
COSMOS 252 DEB * (NORAD ID 3938) 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 3938) 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 25,721 km/h (15,982 mph) — roughly 7.14 km/s. It completes 12.56 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 7.14 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.