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FREGAT DEB

NORAD 45648 Debris LEO 2011-037AQ
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
336 km
Apogee
1540 km
Inclination
51.4°
Period
103.8 min
Mean Motion
13.87304477 rev/day
TLE Epoch
2026-06-20 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude938 km
Orbital Velocity26,585 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.87
Eccentricity0.0824
Semi-Major Axis7,309 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2011-07-18
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2011-037AQ
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
FREGAT DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2011-07-18 from Baikonur, Kazakhstan on the RadioAstron launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 336 km and 1,540 km with an inclination of 51.4°. It travels at approximately 26,585 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.87 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, FREGAT 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
FREGAT DEB orbits at an average altitude of 938 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of FREGAT DEB’s average altitude, there are currently 319 active payloads and 1,120 tracked debris or rocket body fragments. With an inclination of 51.4°, FREGAT DEB passes over latitudes between 51.4°N and 51.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Russia (CIS) operates approximately 1,285 active satellites in total, of which 149 share a similar altitude band with FREGAT DEB.
🔗 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
FREGAT DEB orbits in Low Earth Orbit (LEO) at altitudes between 336 km (perigee) and 1,540 km (apogee), with an average altitude of approximately 938 km. It completes one orbit every 104 minutes, travelling at approximately 26,585 km/h (16,519 mph).
FREGAT DEB (NORAD ID 45648) 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.
FREGAT DEB was launched on 2011-07-18 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT DEB (NORAD ID 45648) 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.
FREGAT DEB travels at approximately 26,585 km/h (16,519 mph) — roughly 7.38 km/s. It completes 13.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.38 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 FREGAT DEB. Read more about debris statistics and the Kessler syndrome.