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BREEZE-M R/B

NORAD 36793 Rocket Body MEO 2010-034B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
5340 km
Apogee
34370 km
Inclination
18.4°
Period
704.7 min
Mean Motion
2.04330782 rev/day
TLE Epoch
2026-06-25 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,855 km
Orbital Velocity14,035 km/h
Velocity3.90 km/s
Orbital Period11 hours 45 minutes
Orbits / Day2.04
Eccentricity0.5535
Semi-Major Axis26,226 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2010-07-10
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2010-034B
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 2010-07-10 from Baikonur, Kazakhstan on the Echostar XV launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 5,340 km and 34,370 km with an inclination of 18.4°. It travels at approximately 14,035 km/h (3.90 km/s), completing one full orbit every 11 hours 45 minutes — that’s roughly 2.04 orbits per day. Its orbital eccentricity of 0.5535 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 19,855 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 1 active payload and 26 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 18.4°, BREEZE-M R/B passes over latitudes between 18.4°N and 18.4°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 5,340 km (perigee) and 34,370 km (apogee), with an average altitude of approximately 19,855 km. It completes one orbit every 11 hours 45 minutes, travelling at approximately 14,035 km/h (8,721 mph).
BREEZE-M R/B (NORAD ID 36793) 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 2010-07-10 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 36793) 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 14,035 km/h (8,721 mph) — roughly 3.90 km/s. It completes 2.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.