FREGAT R/B
NORAD 40130
Rocket Body
MEO
2014-050C
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MEO · NORAD 40130
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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
12764 km
Apogee
26826 km
Inclination
48.4°
Period
702.3 min
Mean Motion
2.05032036 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,795 km
Orbital Velocity14,051 km/h
Velocity3.90 km/s
Orbital Period11 hours 42 minutes
Orbits / Day2.05
Eccentricity0.2687
Semi-Major Axis26,166 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-08-22
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2014-050C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FREGAT R/B is a spent rocket body associated with Russia (CIS), launched on 2014-08-22 from Guiana Space Centre, Kourou on the GalileoSat 5-6 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 12,764 km and 26,826 km with an inclination of 48.4°. It travels at approximately 14,051 km/h (3.90 km/s), completing one full orbit every 11 hours 42 minutes — that’s roughly 2.05 orbits per day. Its orbital eccentricity of 0.2687 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like FREGAT R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
FREGAT R/B orbits at an average altitude of 19,795 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 R/B’s average altitude, there are currently 2 active payloads and 12 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 48.4°, FREGAT R/B passes over latitudes between 48.4°N and 48.4°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 1,286 active satellites in total, of which 2 share a similar altitude band with FREGAT R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
FREGAT R/B orbits in Medium Earth Orbit (MEO) at altitudes between 12,764 km (perigee) and 26,826 km (apogee), with an average altitude of approximately 19,795 km. It completes one orbit every 11 hours 42 minutes, travelling at approximately 14,051 km/h (8,731 mph).
FREGAT R/B (NORAD ID 40130) is a spent rocket body — the upper stage of a launch vehicle attributed to Russia (CIS). It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
FREGAT R/B was launched on 2014-08-22 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 40130) 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 R/B travels at approximately 14,051 km/h (8,731 mph) — roughly 3.90 km/s. It completes 2.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.