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BREEZE-M R/B

NORAD 34942 Rocket Body MEO 2009-027B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
14276 km
Apogee
35436 km
Inclination
8.3°
Period
915.6 min
Mean Motion
1.57274517 rev/day
TLE Epoch
2026-06-25 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude24,856 km
Orbital Velocity12,862 km/h
Velocity3.57 km/s
Orbital Period15 hours 16 minutes
Orbits / Day1.57
Eccentricity0.3388
Semi-Major Axis31,227 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2009-05-16
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2009-027B
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 2009-05-16 from Baikonur, Kazakhstan on the Indostar II/Protostar II launch. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 14,276 km and 35,436 km with an inclination of 8.3°. It travels at approximately 12,862 km/h (3.57 km/s), completing one full orbit every 15 hours 16 minutes — that’s roughly 1.57 orbits per day. Its orbital eccentricity of 0.3388 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 24,856 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 8.3°, BREEZE-M R/B passes over latitudes between 8.3°N and 8.3°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 14,276 km (perigee) and 35,436 km (apogee), with an average altitude of approximately 24,856 km. It completes one orbit every 15 hours 16 minutes, travelling at approximately 12,862 km/h (7,992 mph).
BREEZE-M R/B (NORAD ID 34942) 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 2009-05-16 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 34942) 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 12,862 km/h (7,992 mph) — roughly 3.57 km/s. It completes 1.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.