BREEZE-M DEB
NORAD 38884
Debris
MEO
2012-044R
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MEO · NORAD 38884
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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
260 km
Apogee
3302 km
Inclination
50.0°
Period
122.3 min
Mean Motion
11.77955085 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,781 km
Orbital Velocity25,173 km/h
Velocity6.99 km/s
Orbital Period2 hours 2 minutes
Orbits / Day11.78
Eccentricity0.1866
Semi-Major Axis8,152 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2012-08-06
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2012-044R
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 2012-08-06 from Baikonur, Kazakhstan on the Telkom-3 launch. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 260 km and 3,302 km with an inclination of 50.0°. It travels at approximately 25,173 km/h (6.99 km/s), completing one full orbit every 2 hours 2 minutes — that’s roughly 11.78 orbits per day. Its orbital eccentricity of 0.1866 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. 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 1,781 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 7 active payloads and 30 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 50.0°, BREEZE-M DEB passes over latitudes between 50.0°N and 50.0°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 260 km (perigee) and 3,302 km (apogee), with an average altitude of approximately 1,781 km. It completes one orbit every 2 hours 2 minutes, travelling at approximately 25,173 km/h (15,642 mph).
BREEZE-M DEB (NORAD ID 38884) 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 2012-08-06 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks BREEZE-M DEB (NORAD ID 38884) 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 25,173 km/h (15,642 mph) — roughly 6.99 km/s. It completes 11.78 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 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 6.99 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.