BREEZE-M R/B
NORAD 40883
Rocket Body
HEO
2015-042B
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HEO · NORAD 40883
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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
1762 km
Apogee
64655 km
Inclination
28.7°
Period
1306.4 min
Mean Motion
1.10225862 rev/day
TLE Epoch
2026-06-21 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude33,209 km
Orbital Velocity11,424 km/h
Velocity3.17 km/s
Orbital Period21 hours 46 minutes
Orbits / Day1.10
Eccentricity0.7945
Semi-Major Axis39,580 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2015-08-28
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2015-042B
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 2015-08-28 from Baikonur, Kazakhstan on the Inmarsat 5F3 launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 1,762 km and 64,655 km with an inclination of 28.7°. It travels at approximately 11,424 km/h (3.17 km/s), completing one full orbit every 21 hours 46 minutes — that’s roughly 1.10 orbits per day. Its orbital eccentricity of 0.7945 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 follows a Highly Elliptical Orbit, sweeping between 1,762 km (perigee) and 64,655 km (apogee). It spends most of its 21 hours 46 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 28.7°, BREEZE-M R/B passes over latitudes between 28.7°N and 28.7°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. 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 follows a Highly Elliptical Orbit, swinging between 1,762 km (perigee) and 64,655 km (apogee). It spends most of its 21 hours 46 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
BREEZE-M R/B (NORAD ID 40883) 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 2015-08-28 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks BREEZE-M R/B (NORAD ID 40883) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 11,424 km/h (3.17 km/s), completing one revolution every 21 hours 46 minutes. Learn more about highly elliptical orbits.