BREEZE-M R/B
NORAD 36398
Rocket Body
MEO
2010-006B
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MEO · NORAD 36398
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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
37896 km
Apogee
42091 km
Inclination
13.9°
Period
1656.3 min
Mean Motion
0.86942240 rev/day
TLE Epoch
2026-06-24 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude39,994 km
Orbital Velocity10,555 km/h
Velocity2.93 km/s
Orbital Period27.6 hours
Orbits / Day0.87
Eccentricity0.0452
Semi-Major Axis46,365 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2010-02-12
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2010-006B
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 2010-02-12 from Baikonur, Kazakhstan on the IS-16 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 37,896 km and 42,091 km with an inclination of 13.9°. It travels at approximately 10,555 km/h (2.93 km/s), completing one full orbit every 27.6 hours — that’s roughly 0.87 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. 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 39,994 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 13.9°, BREEZE-M R/B passes over latitudes between 13.9°N and 13.9°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 37,896 km (perigee) and 42,091 km (apogee), with an average altitude of approximately 39,994 km. It completes one orbit every 27.6 hours, travelling at approximately 10,555 km/h (6,559 mph).
BREEZE-M R/B (NORAD ID 36398) 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 2010-02-12 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 36398) 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 10,555 km/h (6,559 mph) — roughly 2.93 km/s. It completes 0.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.