FREGAT DEB
NORAD 40078
Debris
LEO
2014-037K
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LEO · NORAD 40078
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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
614 km
Apogee
800 km
Inclination
98.1°
Period
98.9 min
Mean Motion
14.55659633 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude707 km
Orbital Velocity27,016 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.56
Eccentricity0.0131
Semi-Major Axis7,078 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-07-08
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-037K
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
FREGAT DEB is a tracked piece of space debris attributed to Russia (CIS), launched on 2014-07-08 from Baikonur, Kazakhstan on the Soyuz Rideshare 3 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 614 km and 800 km with an inclination of 98.1°. It travels at approximately 27,016 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.56 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 707 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of FREGAT DEB’s average altitude, there are currently 251 active payloads and 1,510 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, FREGAT DEB passes over latitudes between 98.1°N and 98.1°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,285 active satellites in total, of which 9 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 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 707 km altitude. Its 98.1° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 99 minutes, travelling at 27,016 km/h.
FREGAT DEB (NORAD ID 40078) 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 2014-07-08 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT DEB (NORAD ID 40078) 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 27,016 km/h (16,787 mph) — roughly 7.50 km/s. It completes 14.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.50 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.