BREEZE-M R/B
NORAD 64468
Rocket Body
HEO
2025-131B
CONNECTING…
HEO · NORAD 64468
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
18837 km
Apogee
50481 km
Inclination
0.2°
Period
1378.9 min
Mean Motion
1.04431882 rev/day
TLE Epoch
2026-06-17 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,659 km
Orbital Velocity11,221 km/h
Velocity3.12 km/s
Orbital Period22 hours 59 minutes
Orbits / Day1.04
Eccentricity0.3856
Semi-Major Axis41,030 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2025-06-19
Launch Site
PKMTR
Int'l Designator
2025-131B
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 2025-06-19 from PKMTR. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 18,837 km and 50,481 km with an inclination of 0.2°. It travels at approximately 11,221 km/h (3.12 km/s), completing one full orbit every 22 hours 59 minutes — that’s roughly 1.04 orbits per day. Its orbital eccentricity of 0.3856 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 18,837 km (perigee) and 50,481 km (apogee). It spends most of its 22 hours 59 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. Within ±50 km of BREEZE-M R/B’s average altitude, there are currently 0 active payloads and 5 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 0.2°, BREEZE-M R/B passes over latitudes between 0.2°N and 0.2°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,284 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 18,837 km (perigee) and 50,481 km (apogee). It spends most of its 22 hours 59 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 64468) 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 2025-06-19 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks BREEZE-M R/B (NORAD ID 64468) 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 11,221 km/h (3.12 km/s), completing one revolution every 22 hours 59 minutes. Learn more about highly elliptical orbits.