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FREGAT R/B

NORAD 39192 Rocket Body MEO 2013-031E
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
7666 km
Apogee
7689 km
Inclination
0.2°
Period
276.4 min
Mean Motion
5.20984079 rev/day
TLE Epoch
2026-06-25 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,678 km
Orbital Velocity19,176 km/h
Velocity5.33 km/s
Orbital Period4 hours 36 minutes
Orbits / Day5.21
Eccentricity0.0008
Semi-Major Axis14,049 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2013-06-25
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2013-031E
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 2013-06-25 from Guiana Space Centre, Kourou on the O3b SV1/SV2/SV4/SV5 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 7,666 km and 7,689 km with an inclination of 0.2°. It travels at approximately 19,176 km/h (5.33 km/s), completing one full orbit every 4 hours 36 minutes — that’s roughly 5.21 orbits per day. 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 7,678 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 0 active payloads and 10 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 0.2°, FREGAT R/B passes over latitudes between 0.2°N and 0.2°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Russia (CIS) operates approximately 1,286 active satellites in total.
🔗 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 7,666 km (perigee) and 7,689 km (apogee), with an average altitude of approximately 7,678 km. It completes one orbit every 4 hours 36 minutes, travelling at approximately 19,176 km/h (11,915 mph).
FREGAT R/B (NORAD ID 39192) 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 2013-06-25 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 39192) 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 19,176 km/h (11,915 mph) — roughly 5.33 km/s. It completes 5.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 10 sunrises and sunsets every 24 hours.