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BREEZE-M DEB (ADAPTOR)

NORAD 37787 Debris MEO 2011-035E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
3686 km
Apogee
35742 km
Inclination
24.6°
Period
699.1 min
Mean Motion
2.05985155 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,714 km
Orbital Velocity14,073 km/h
Velocity3.91 km/s
Orbital Period11 hours 39 minutes
Orbits / Day2.06
Eccentricity0.6145
Semi-Major Axis26,085 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2011-07-15
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2011-035E
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
BREEZE-M DEB (ADAPTOR) is a tracked piece of space debris attributed to Russia (CIS), launched on 2011-07-15 from Baikonur, Kazakhstan on the SES-3 launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,686 km and 35,742 km with an inclination of 24.6°. It travels at approximately 14,073 km/h (3.91 km/s), completing one full orbit every 11 hours 39 minutes — that’s roughly 2.06 orbits per day. Its orbital eccentricity of 0.6145 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, BREEZE-M DEB (ADAPTOR) 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 (ADAPTOR) orbits at an average altitude of 19,714 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 DEB (ADAPTOR)’s average altitude, there are currently 1 active payload and 11 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 24.6°, BREEZE-M DEB (ADAPTOR) passes over latitudes between 24.6°N and 24.6°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 1,285 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 (ADAPTOR) orbits in Medium Earth Orbit (MEO) at altitudes between 3,686 km (perigee) and 35,742 km (apogee), with an average altitude of approximately 19,714 km. It completes one orbit every 11 hours 39 minutes, travelling at approximately 14,073 km/h (8,744 mph).
BREEZE-M DEB (ADAPTOR) (NORAD ID 37787) 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 (ADAPTOR) was launched on 2011-07-15 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 (ADAPTOR) (NORAD ID 37787) 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 (ADAPTOR) travels at approximately 14,073 km/h (8,744 mph) — roughly 3.91 km/s. It completes 2.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
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 3.91 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 (ADAPTOR). Read more about debris statistics and the Kessler syndrome.