COSMOS 397 DEB
NORAD 5272
Debris
LEO
1971-015BB
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LEO · NORAD 5272
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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
542 km
Apogee
1648 km
Inclination
65.5°
Period
107.2 min
Mean Motion
13.43894035 rev/day
TLE Epoch
2026-09-18 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,095 km
Orbital Velocity26,304 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.44
Eccentricity0.0741
Semi-Major Axis7,466 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1971-02-25
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1971-015BB
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 397 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1971-02-25 from Baikonur Cosmodrome, Kazakhstan on the I2P launch. After more than 55 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 542 km and 1,648 km with an inclination of 65.5°. It travels at approximately 26,304 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.44 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, COSMOS 397 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 397 DEB orbits at an average altitude of 1,095 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 397 DEB’s average altitude, there are currently 303 active payloads and 525 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 65.5°, COSMOS 397 DEB passes over latitudes between 65.5°N and 65.5°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 1,537 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 397 DEB orbits in Low Earth Orbit (LEO) at altitudes between 542 km (perigee) and 1,648 km (apogee), with an average altitude of approximately 1,095 km. It completes one orbit every 107 minutes, travelling at approximately 26,304 km/h (16,345 mph).
COSMOS 397 DEB (NORAD ID 5272) 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 397 DEB was launched on 1971-02-25 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 397 DEB (NORAD ID 5272) 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 397 DEB travels at approximately 26,304 km/h (16,345 mph) — roughly 7.31 km/s. It completes 13.44 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 7.31 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 397 DEB. Read more about debris statistics and the Kessler syndrome.