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COSMOS 2251 DEB

NORAD 34823 Debris LEO 1993-036ABN
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
599 km
Apogee
815 km
Inclination
74.0°
Period
98.9 min
Mean Motion
14.55737274 rev/day
TLE Epoch
2026-06-25 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude707 km
Orbital Velocity27,016 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.56
Eccentricity0.0153
Semi-Major Axis7,078 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1993-06-16
Launch Site
PKMTR
Int'l Designator
1993-036ABN
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
COSMOS 2251 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 1993-06-16 from PKMTR on the Strela-2M launch. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 599 km and 815 km with an inclination of 74.0°. It travels at approximately 27,016 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, COSMOS 2251 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 2251 DEB orbits at an average altitude of 707 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 2251 DEB’s average altitude, there are currently 250 active payloads and 1,526 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 74.0°, COSMOS 2251 DEB passes over latitudes between 74.0°N and 74.0°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 1,287 active satellites in total, of which 8 share a similar altitude band with COSMOS 2251 DEB.
🔗 Cosmos–Iridium Collision Debris

This debris object was created by the first accidental hypervelocity collision between two intact satellites — Cosmos 2251 (defunct, Russia) and Iridium 33 (active, USA) — on 10 February 2009 at approximately 790 km altitude. The collision occurred at a relative velocity of about 11.7 km/s and produced over 2,300 trackable fragments, many of which remain in orbit.

❓ Frequently Asked Questions
COSMOS 2251 DEB orbits in Low Earth Orbit (LEO) at altitudes between 599 km (perigee) and 815 km (apogee), with an average altitude of approximately 707 km. It completes one orbit every 99 minutes, travelling at approximately 27,016 km/h (16,787 mph).
COSMOS 2251 DEB (NORAD ID 34823) 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 2251 DEB was launched on 1993-06-16 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2251 DEB (NORAD ID 34823) 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 2251 DEB travels at approximately 27,016 km/h (16,787 mph) — roughly 7.50 km/s. It completes 14.56 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 7.50 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 2251 DEB. Read more about debris statistics and the Kessler syndrome.