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BREEZE-M R/B

NORAD 43868 Rocket Body MEO 2018-107B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35502 km
Apogee
42057 km
Inclination
7.5°
Period
1591.7 min
Mean Motion
0.90469931 rev/day
TLE Epoch
2026-06-25 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude38,780 km
Orbital Velocity10,696 km/h
Velocity2.97 km/s
Orbital Period26.5 hours
Orbits / Day0.90
Eccentricity0.0726
Semi-Major Axis45,151 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2018-12-21
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2018-107B
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 2018-12-21 from Baikonur, Kazakhstan on the Blagovest 13L launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 35,502 km and 42,057 km with an inclination of 7.5°. It travels at approximately 10,696 km/h (2.97 km/s), completing one full orbit every 26.5 hours — that’s roughly 0.90 orbits per day. 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 orbits at an average altitude of 38,780 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. With an inclination of 7.5°, BREEZE-M R/B passes over latitudes between 7.5°N and 7.5°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 35,502 km (perigee) and 42,057 km (apogee), with an average altitude of approximately 38,780 km. It completes one orbit every 26.5 hours, travelling at approximately 10,696 km/h (6,646 mph).
BREEZE-M R/B (NORAD ID 43868) 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 2018-12-21 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 43868) 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 10,696 km/h (6,646 mph) — roughly 2.97 km/s. It completes 0.90 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.