Skip to content
Home Library Satellite Directory FREGAT DEB

FREGAT DEB

NORAD 46406 Debris MEO 2011-037LM
CONNECTING… MEO · NORAD 46406
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
785 km
Apogee
4406 km
Inclination
51.6°
Period
141.0 min
Mean Motion
10.21288518 rev/day
TLE Epoch
2026-06-19 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,596 km
Orbital Velocity24,003 km/h
Velocity6.67 km/s
Orbital Period2 hours 21 minutes
Orbits / Day10.21
Eccentricity0.2019
Semi-Major Axis8,967 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2011-07-18
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2011-037LM
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 Medium Earth Orbit (MEO) at altitudes between 785 km and 4,406 km with an inclination of 51.6°. It travels at approximately 24,003 km/h (6.67 km/s), completing one full orbit every 2 hours 21 minutes — that’s roughly 10.21 orbits per day. Its orbital eccentricity of 0.2019 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 2,596 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 FREGAT DEB’s average altitude, there are currently 0 active payloads and 6 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 51.6°, FREGAT DEB passes over latitudes between 51.6°N and 51.6°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.
🔗 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 Medium Earth Orbit (MEO) at altitudes between 785 km (perigee) and 4,406 km (apogee), with an average altitude of approximately 2,596 km. It completes one orbit every 2 hours 21 minutes, travelling at approximately 24,003 km/h (14,915 mph).
FREGAT DEB (NORAD ID 46406) 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT DEB (NORAD ID 46406) 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 24,003 km/h (14,915 mph) — roughly 6.67 km/s. It completes 10.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 20 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 6.67 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.