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BREEZE M R/B

NORAD 36517 Rocket Body MEO 2010-016B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
28267 km
Apogee
33603 km
Inclination
8.1°
Period
1195.5 min
Mean Motion
1.20450874 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude30,935 km
Orbital Velocity11,767 km/h
Velocity3.27 km/s
Orbital Period19 hours 56 minutes
Orbits / Day1.20
Eccentricity0.0715
Semi-Major Axis37,306 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2010-04-24
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2010-016B
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 2010-04-24 from Baikonur, Kazakhstan on the SES-1 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 28,267 km and 33,603 km with an inclination of 8.1°. It travels at approximately 11,767 km/h (3.27 km/s), completing one full orbit every 19 hours 56 minutes — that’s roughly 1.20 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 30,935 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 0 active payloads and 3 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 8.1°, BREEZE M R/B passes over latitudes between 8.1°N and 8.1°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 28,267 km (perigee) and 33,603 km (apogee), with an average altitude of approximately 30,935 km. It completes one orbit every 19 hours 56 minutes, travelling at approximately 11,767 km/h (7,312 mph).
BREEZE M R/B (NORAD ID 36517) 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 2010-04-24 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 36517) 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 11,767 km/h (7,312 mph) — roughly 3.27 km/s. It completes 1.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.