COSMOS 2491 DEB
NORAD 57553
Debris
LEO
2013-076AQ
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LEO · NORAD 57553
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
1428 km
Apogee
1499 km
Inclination
82.5°
Period
115.2 min
Mean Motion
12.50316830 rev/day
TLE Epoch
2026-06-15 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,464 km
Orbital Velocity25,678 km/h
Velocity7.13 km/s
Orbital Period115 minutes
Orbits / Day12.50
Eccentricity0.0045
Semi-Major Axis7,835 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-12-25
Launch Site
PKMTR
Int'l Designator
2013-076AQ
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
COSMOS 2491 DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2013-12-25 from PKMTR. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 1,428 km and 1,499 km with an inclination of 82.5°. It travels at approximately 25,678 km/h (7.13 km/s), completing one full orbit every 115 minutes — that’s roughly 12.50 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, COSMOS 2491 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 2491 DEB orbits at an average altitude of 1,464 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of COSMOS 2491 DEB’s average altitude, there are currently 334 active payloads and 241 tracked debris or rocket body fragments. With an inclination of 82.5°, COSMOS 2491 DEB passes over latitudes between 82.5°N and 82.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,286 active satellites in total, of which 323 share a similar altitude band with COSMOS 2491 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 2491 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,428 km (perigee) and 1,499 km (apogee), with an average altitude of approximately 1,464 km. It completes one orbit every 115 minutes, travelling at approximately 25,678 km/h (15,956 mph).
COSMOS 2491 DEB (NORAD ID 57553) 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 2491 DEB was launched on 2013-12-25 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks COSMOS 2491 DEB (NORAD ID 57553) 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 2491 DEB travels at approximately 25,678 km/h (15,956 mph) — roughly 7.13 km/s. It completes 12.50 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.13 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 2491 DEB. Read more about debris statistics and the Kessler syndrome.