COSMOS 397 DEB *
NORAD 5414
Debris
LEO
1971-015BL
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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
823 km
Apogee
943 km
Inclination
66.8°
Period
102.6 min
Mean Motion
14.03080612 rev/day
TLE Epoch
2026-09-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude883 km
Orbital Velocity26,686 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.03
Eccentricity0.0083
Semi-Major Axis7,254 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1971-02-25
Launch Site
Baikonur Cosmodrome, Kazakhstan
Int'l Designator
1971-015BL
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 823 km and 943 km with an inclination of 66.8°. It travels at approximately 26,686 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.03 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 883 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 240 active payloads and 1,836 tracked debris or rocket body fragments. With an inclination of 66.8°, COSMOS 397 DEB * passes over latitudes between 66.8°N and 66.8°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 72 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 823 km (perigee) and 943 km (apogee), with an average altitude of approximately 883 km. It completes one orbit every 103 minutes, travelling at approximately 26,686 km/h (16,582 mph).
COSMOS 397 DEB * (NORAD ID 5414) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 397 DEB * (NORAD ID 5414) 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 26,686 km/h (16,582 mph) — roughly 7.41 km/s. It completes 14.03 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 7.41 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.