BREEZE-M DEB
NORAD 41548
Debris
GEO
2015-075J
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GEO · NORAD 41548
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
33709 km
Apogee
36803 km
Inclination
8.7°
Period
1409.1 min
Mean Motion
1.02194159 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,256 km
Orbital Velocity11,140 km/h
Velocity3.09 km/s
Orbital Period23 hours 29 minutes
Orbits / Day1.02
Eccentricity0.0372
Semi-Major Axis41,627 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2015-12-13
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2015-075J
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
BREEZE-M DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2015-12-13 from Baikonur, Kazakhstan on the Garpun No. 12L launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 33,709 km and 36,803 km with an inclination of 8.7°. It travels at approximately 11,140 km/h (3.09 km/s), completing one full orbit every 23 hours 29 minutes — that’s roughly 1.02 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, BREEZE-M DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
BREEZE-M DEB occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 8.7°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of BREEZE-M DEB’s average altitude, there are currently 3 active payloads and 14 tracked debris or rocket body fragments. Russia (CIS) operates approximately 1,285 active satellites in total.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
BREEZE-M DEB orbits at approximately 35,256 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,140 km/h — it just keeps pace with the ground below. With an inclination of 8.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
BREEZE-M DEB (NORAD ID 41548) is a piece of tracked orbital debris attributed to Russia (CIS). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
BREEZE-M DEB was launched on 2015-12-13 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 DEB (NORAD ID 41548) 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 DEB travels at approximately 11,140 km/h (6,922 mph) — roughly 3.09 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 3.09 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like BREEZE-M DEB. Read more about debris statistics and the Kessler syndrome.