BREEZE-M DEB
NORAD 38590
Debris
MEO
2008-011AM
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MEO · NORAD 38590
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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
1433 km
Apogee
27502 km
Inclination
48.9°
Period
499.2 min
Mean Motion
2.88454980 rev/day
TLE Epoch
2026-06-20 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude14,468 km
Orbital Velocity15,745 km/h
Velocity4.37 km/s
Orbital Period8 hours 19 minutes
Orbits / Day2.88
Eccentricity0.6255
Semi-Major Axis20,839 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2008-03-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2008-011AM
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
BREEZE-M DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2008-03-14 from Baikonur, Kazakhstan on the Americom 14 launch. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,433 km and 27,502 km with an inclination of 48.9°. It travels at approximately 15,745 km/h (4.37 km/s), completing one full orbit every 8 hours 19 minutes — that’s roughly 2.88 orbits per day. Its orbital eccentricity of 0.6255 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, BREEZE-M 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
BREEZE-M DEB orbits at an average altitude of 14,468 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of BREEZE-M DEB’s average altitude, there are currently 0 active payloads and 5 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 48.9°, BREEZE-M DEB passes over latitudes between 48.9°N and 48.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Russia (CIS) operates approximately 1,285 active satellites in total.
🔗 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
BREEZE-M DEB orbits in Medium Earth Orbit (MEO) at altitudes between 1,433 km (perigee) and 27,502 km (apogee), with an average altitude of approximately 14,468 km. It completes one orbit every 8 hours 19 minutes, travelling at approximately 15,745 km/h (9,783 mph).
BREEZE-M DEB (NORAD ID 38590) 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.
BREEZE-M DEB was launched on 2008-03-14 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks BREEZE-M DEB (NORAD ID 38590) 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.
BREEZE-M DEB travels at approximately 15,745 km/h (9,783 mph) — roughly 4.37 km/s. It completes 2.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 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 4.37 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 BREEZE-M DEB. Read more about debris statistics and the Kessler syndrome.