BREEZE-M R/B
NORAD 37934
Rocket Body
MEO
2011-069B
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MEO · NORAD 37934
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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
11884 km
Apogee
34302 km
Inclination
1.5°
Period
839.2 min
Mean Motion
1.71597668 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,093 km
Orbital Velocity13,241 km/h
Velocity3.68 km/s
Orbital Period13 hours 59 minutes
Orbits / Day1.72
Eccentricity0.3804
Semi-Major Axis29,464 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2011-11-25
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2011-069B
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 2011-11-25 from Baikonur, Kazakhstan on the Asiasat 7 launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 11,884 km and 34,302 km with an inclination of 1.5°. It travels at approximately 13,241 km/h (3.68 km/s), completing one full orbit every 13 hours 59 minutes — that’s roughly 1.72 orbits per day. Its orbital eccentricity of 0.3804 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 23,093 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 0 active payloads and 6 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 1.5°, BREEZE-M R/B passes over latitudes between 1.5°N and 1.5°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 11,884 km (perigee) and 34,302 km (apogee), with an average altitude of approximately 23,093 km. It completes one orbit every 13 hours 59 minutes, travelling at approximately 13,241 km/h (8,228 mph).
BREEZE-M R/B (NORAD ID 37934) 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 2011-11-25 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 37934) 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 13,241 km/h (8,228 mph) — roughly 3.68 km/s. It completes 1.72 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.