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BREEZE-M R/B

NORAD 44626 Rocket Body HEO 2019-067C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
9138 km
Apogee
66239 km
Inclination
23.8°
Period
1534.3 min
Mean Motion
0.93851075 rev/day
TLE Epoch
2026-06-25 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,689 km
Orbital Velocity10,828 km/h
Velocity3.01 km/s
Orbital Period25.6 hours
Orbits / Day0.94
Eccentricity0.6480
Semi-Major Axis44,060 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2019-10-09
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2019-067C
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 2019-10-09 from Baikonur, Kazakhstan on the MEV-1/Eutelsat-5WB launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 9,138 km and 66,239 km with an inclination of 23.8°. It travels at approximately 10,828 km/h (3.01 km/s), completing one full orbit every 25.6 hours — that’s roughly 0.94 orbits per day. Its orbital eccentricity of 0.6480 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 follows a Highly Elliptical Orbit, sweeping between 9,138 km (perigee) and 66,239 km (apogee). It spends most of its 25.6 hours 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. Within ±50 km of BREEZE-M R/B’s average altitude, there are currently 1 active payload 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 23.8°, BREEZE-M R/B passes over latitudes between 23.8°N and 23.8°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 9,138 km (perigee) and 66,239 km (apogee). It spends most of its 25.6 hours 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 44626) 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 2019-10-09 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 44626) 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 10,828 km/h (3.01 km/s), completing one revolution every 25.6 hours. Learn more about highly elliptical orbits.