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BREEZE-M R/B

NORAD 28360 Rocket Body MEO 2004-022C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
4237 km
Apogee
35965 km
Inclination
24.0°
Period
714.7 min
Mean Motion
2.01484751 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,101 km
Orbital Velocity13,969 km/h
Velocity3.88 km/s
Orbital Period11 hours 55 minutes
Orbits / Day2.01
Eccentricity0.5993
Semi-Major Axis26,472 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2004-06-16
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2004-022C
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 2004-06-16 from Baikonur, Kazakhstan on the INTELSAT 10-02 launch. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 4,237 km and 35,965 km with an inclination of 24.0°. It travels at approximately 13,969 km/h (3.88 km/s), completing one full orbit every 11 hours 55 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.5993 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 20,101 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 5 active payloads and 18 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 24.0°, BREEZE-M R/B passes over latitudes between 24.0°N and 24.0°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, of which 4 share a similar altitude band with BREEZE-M R/B.
🔗 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 4,237 km (perigee) and 35,965 km (apogee), with an average altitude of approximately 20,101 km. It completes one orbit every 11 hours 55 minutes, travelling at approximately 13,969 km/h (8,680 mph).
BREEZE-M R/B (NORAD ID 28360) 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 2004-06-16 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 28360) 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 13,969 km/h (8,680 mph) — roughly 3.88 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.