BREEZE-M DEB
NORAD 43414
Debris
MEO
2014-007D
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MEO · NORAD 43414
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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
8282 km
Apogee
34149 km
Inclination
14.7°
Period
760.3 min
Mean Motion
1.89405164 rev/day
TLE Epoch
2026-06-20 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude21,216 km
Orbital Velocity13,684 km/h
Velocity3.80 km/s
Orbital Period12 hours 40 minutes
Orbits / Day1.89
Eccentricity0.4688
Semi-Major Axis27,587 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-02-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-007D
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 2014-02-14 from Baikonur, Kazakhstan on the Turksat 4A launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 8,282 km and 34,149 km with an inclination of 14.7°. It travels at approximately 13,684 km/h (3.80 km/s), completing one full orbit every 12 hours 40 minutes — that’s roughly 1.89 orbits per day. Its orbital eccentricity of 0.4688 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 21,216 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 8 active payloads and 14 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 14.7°, BREEZE-M DEB passes over latitudes between 14.7°N and 14.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 8,282 km (perigee) and 34,149 km (apogee), with an average altitude of approximately 21,216 km. It completes one orbit every 12 hours 40 minutes, travelling at approximately 13,684 km/h (8,503 mph).
BREEZE-M DEB (NORAD ID 43414) 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 2014-02-14 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks BREEZE-M DEB (NORAD ID 43414) 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 13,684 km/h (8,503 mph) — roughly 3.80 km/s. It completes 1.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 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 3.80 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.