BREEZE-M R/B
NORAD 40346
Rocket Body
MEO
2014-082B
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MEO · NORAD 40346
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🛰️ Orbital Parameters
Perigee
30346 km
Apogee
35544 km
Inclination
8.7°
Period
1293.4 min
Mean Motion
1.11335253 rev/day
TLE Epoch
2026-06-25 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude32,945 km
Orbital Velocity11,463 km/h
Velocity3.18 km/s
Orbital Period21 hours 33 minutes
Orbits / Day1.11
Eccentricity0.0661
Semi-Major Axis39,316 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-12-15
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-082B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
BREEZE-M R/B is a spent rocket body associated with Russia (CIS), launched on 2014-12-15 from Baikonur, Kazakhstan on the Yamal-401 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 30,346 km and 35,544 km with an inclination of 8.7°. It travels at approximately 11,463 km/h (3.18 km/s), completing one full orbit every 21 hours 33 minutes — that’s roughly 1.11 orbits per day. 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 32,945 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. With an inclination of 8.7°, BREEZE-M R/B passes over latitudes between 8.7°N and 8.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,286 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 30,346 km (perigee) and 35,544 km (apogee), with an average altitude of approximately 32,945 km. It completes one orbit every 21 hours 33 minutes, travelling at approximately 11,463 km/h (7,123 mph).
BREEZE-M R/B (NORAD ID 40346) 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 2014-12-15 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 40346) 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 11,463 km/h (7,123 mph) — roughly 3.18 km/s. It completes 1.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.