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BREEZE-M R/B

NORAD 28869 Rocket Body MEO 2005-036B
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
3223 km
Apogee
35417 km
Inclination
9.2°
Period
683.3 min
Mean Motion
2.10741091 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,320 km
Orbital Velocity14,180 km/h
Velocity3.94 km/s
Orbital Period11 hours 23 minutes
Orbits / Day2.11
Eccentricity0.6266
Semi-Major Axis25,691 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2005-09-08
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2005-036B
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 2005-09-08 from Baikonur, Kazakhstan on the Anik F1R launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,223 km and 35,417 km with an inclination of 9.2°. It travels at approximately 14,180 km/h (3.94 km/s), completing one full orbit every 11 hours 23 minutes — that’s roughly 2.11 orbits per day. Its orbital eccentricity of 0.6266 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 19,320 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 9.2°, BREEZE-M R/B passes over latitudes between 9.2°N and 9.2°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 3,223 km (perigee) and 35,417 km (apogee), with an average altitude of approximately 19,320 km. It completes one orbit every 11 hours 23 minutes, travelling at approximately 14,180 km/h (8,811 mph).
BREEZE-M R/B (NORAD ID 28869) 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 2005-09-08 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 28869) 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 14,180 km/h (8,811 mph) — roughly 3.94 km/s. It completes 2.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.