BREEZE-M R/B
NORAD 39376
Rocket Body
GEO
2013-062B
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GEO · NORAD 39376
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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
33762 km
Apogee
35673 km
Inclination
9.4°
Period
1381.8 min
Mean Motion
1.04209681 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,718 km
Orbital Velocity11,213 km/h
Velocity3.11 km/s
Orbital Period23 hours 2 minutes
Orbits / Day1.04
Eccentricity0.0233
Semi-Major Axis41,089 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-11-11
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2013-062B
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 2013-11-11 from Baikonur, Kazakhstan on the Globus-1M No. 13L launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 33,762 km and 35,673 km with an inclination of 9.4°. It travels at approximately 11,213 km/h (3.11 km/s), completing one full orbit every 23 hours 2 minutes — that’s roughly 1.04 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 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 9.4°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. 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 at approximately 34,718 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,213 km/h — it just keeps pace with the ground below. With an inclination of 9.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
BREEZE-M R/B (NORAD ID 39376) 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 2013-11-11 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 39376) 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 11,213 km/h (6,967 mph) — roughly 3.11 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.