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COSMOS 397 DEB

NORAD 5155 Debris LEO 1971-015AJ
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
485 km
Apogee
894 km
Inclination
65.3°
Period
98.5 min
Mean Motion
14.61242748 rev/day
TLE Epoch
2026-09-17 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude690 km
Orbital Velocity27,049 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.61
Eccentricity0.0290
Semi-Major Axis7,061 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1971-02-25
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1971-015AJ
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 485 km and 894 km with an inclination of 65.3°. It travels at approximately 27,049 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 690 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of COSMOS 397 DEB’s average altitude, there are currently 335 active payloads and 1,448 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 65.3°, COSMOS 397 DEB passes over latitudes between 65.3°N and 65.3°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 1,537 active satellites in total, of which 20 share a similar altitude band with COSMOS 397 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 397 DEB orbits in Low Earth Orbit (LEO) at altitudes between 485 km (perigee) and 894 km (apogee), with an average altitude of approximately 690 km. It completes one orbit every 99 minutes, travelling at approximately 27,049 km/h (16,808 mph).
COSMOS 397 DEB (NORAD ID 5155) 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 397 DEB (NORAD ID 5155) 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 27,049 km/h (16,808 mph) — roughly 7.51 km/s. It completes 14.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.51 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.