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COSMOS 2251 DEB

NORAD 35824 Debris LEO 1993-036ASW
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
746 km
Apogee
1117 km
Inclination
73.8°
Period
103.7 min
Mean Motion
13.89107930 rev/day
TLE Epoch
2026-06-24 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude932 km
Orbital Velocity26,597 km/h
Velocity7.39 km/s
Orbital Period104 minutes
Orbits / Day13.89
Eccentricity0.0254
Semi-Major Axis7,303 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
1993-06-16
Launch Site
PKMTR
Int'l Designator
1993-036ASW
Object Type
Debris
RCS Size
Small (<0.1 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 746 km and 1,117 km with an inclination of 73.8°. It travels at approximately 26,597 km/h (7.39 km/s), completing one full orbit every 104 minutes — that’s roughly 13.89 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 932 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 2251 DEB’s average altitude, there are currently 294 active payloads and 1,158 tracked debris or rocket body fragments. With an inclination of 73.8°, COSMOS 2251 DEB passes over latitudes between 73.8°N and 73.8°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 1,286 active satellites in total, of which 106 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 746 km (perigee) and 1,117 km (apogee), with an average altitude of approximately 932 km. It completes one orbit every 104 minutes, travelling at approximately 26,597 km/h (16,527 mph).
COSMOS 2251 DEB (NORAD ID 35824) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2251 DEB (NORAD ID 35824) 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 26,597 km/h (16,527 mph) — roughly 7.39 km/s. It completes 13.89 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 7.39 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.