COSMOS 2251 DEB
NORAD 34410
Debris
LEO
1993-036RB
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LEO · NORAD 34410
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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
194 km
Apogee
214 km
Inclination
73.7°
Period
88.6 min
Mean Motion
16.25597099 rev/day
TLE Epoch
2026-08-15 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude204 km
Orbital Velocity28,030 km/h
Velocity7.79 km/s
Orbital Period89 minutes
Orbits / Day16.26
Eccentricity0.0015
Semi-Major Axis6,575 km
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1993-06-16
Launch Site
PKMTR
Int'l Designator
1993-036RB
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 194 km and 214 km with an inclination of 73.7°. It travels at approximately 28,030 km/h (7.79 km/s), completing one full orbit every 89 minutes — that’s roughly 16.26 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is weeks to months. 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 204 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of COSMOS 2251 DEB’s average altitude, there are currently 22 active payloads and 3 tracked debris or rocket body fragments — notable neighbours include STARLINK-1301, STARLINK-1280, STARLINK-1623. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 73.7°, COSMOS 2251 DEB passes over latitudes between 73.7°N and 73.7°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 1,289 active satellites in total.
🔗 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 194 km (perigee) and 214 km (apogee), with an average altitude of approximately 204 km. It completes one orbit every 89 minutes, travelling at approximately 28,030 km/h (17,417 mph).
COSMOS 2251 DEB (NORAD ID 34410) 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: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2251 DEB (NORAD ID 34410) 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 28,030 km/h (17,417 mph) — roughly 7.79 km/s. It completes 16.26 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 33 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 7.79 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.