Skip to content
Home Library Satellite Directory BREEZE-M R/B

BREEZE-M R/B

NORAD 42909 Rocket Body MEO 2017-046C
CONNECTING… MEO · NORAD 42909
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
35399 km
Apogee
42252 km
Inclination
8.7°
Period
1594.1 min
Mean Motion
0.90332630 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude38,826 km
Orbital Velocity10,691 km/h
Velocity2.97 km/s
Orbital Period26.6 hours
Orbits / Day0.90
Eccentricity0.0758
Semi-Major Axis45,197 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2017-08-16
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2017-046C
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 2017-08-16 from Baikonur, Kazakhstan on the Blagovest 11L launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 35,399 km and 42,252 km with an inclination of 8.7°. It travels at approximately 10,691 km/h (2.97 km/s), completing one full orbit every 26.6 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 38,826 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 8.7°, BREEZE-M R/B passes over latitudes between 8.7°N and 8.7°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 35,399 km (perigee) and 42,252 km (apogee), with an average altitude of approximately 38,826 km. It completes one orbit every 26.6 hours, travelling at approximately 10,691 km/h (6,643 mph).
BREEZE-M R/B (NORAD ID 42909) 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 2017-08-16 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 42909) 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 10,691 km/h (6,643 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.