BREEZE-M R/B
NORAD 39123
Rocket Body
MEO
2013-012B
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MEO · NORAD 39123
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
5491 km
Apogee
34034 km
Inclination
17.8°
Period
701.0 min
Mean Motion
2.05414451 rev/day
TLE Epoch
2026-06-25 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,763 km
Orbital Velocity14,060 km/h
Velocity3.91 km/s
Orbital Period11 hours 41 minutes
Orbits / Day2.05
Eccentricity0.5461
Semi-Major Axis26,134 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-03-26
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2013-012B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
BREEZE-M R/B is a spent rocket body associated with Russia (CIS), launched on 2013-03-26 from Baikonur, Kazakhstan on the Satmex 8 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 5,491 km and 34,034 km with an inclination of 17.8°. It travels at approximately 14,060 km/h (3.91 km/s), completing one full orbit every 11 hours 41 minutes — that’s roughly 2.05 orbits per day. Its orbital eccentricity of 0.5461 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like BREEZE-M R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
BREEZE-M R/B orbits at an average altitude of 19,763 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 R/B’s average altitude, there are currently 2 active payloads and 11 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 17.8°, BREEZE-M R/B passes over latitudes between 17.8°N and 17.8°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,286 active satellites in total.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
BREEZE-M R/B orbits in Medium Earth Orbit (MEO) at altitudes between 5,491 km (perigee) and 34,034 km (apogee), with an average altitude of approximately 19,763 km. It completes one orbit every 11 hours 41 minutes, travelling at approximately 14,060 km/h (8,736 mph).
BREEZE-M R/B (NORAD ID 39123) is a spent rocket body — the upper stage of a launch vehicle attributed to Russia (CIS). It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
BREEZE-M R/B was launched on 2013-03-26 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 R/B (NORAD ID 39123) 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 R/B travels at approximately 14,060 km/h (8,736 mph) — roughly 3.91 km/s. It completes 2.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.