FREGAT R/B
NORAD 41176
Rocket Body
MEO
2015-079C
CONNECTING…
MEO · NORAD 41176
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
23525 km
Apogee
23604 km
Inclination
55.8°
Period
859.4 min
Mean Motion
1.67560917 rev/day
TLE Epoch
2026-06-25 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,565 km
Orbital Velocity13,136 km/h
Velocity3.65 km/s
Orbital Period14 hours 19 minutes
Orbits / Day1.68
Eccentricity0.0013
Semi-Major Axis29,936 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2015-12-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2015-079C
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 2015-12-17 from Guiana Space Centre, Kourou on the GalileoSat 11-12 launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 23,525 km and 23,604 km with an inclination of 55.8°. It travels at approximately 13,136 km/h (3.65 km/s), completing one full orbit every 14 hours 19 minutes — that’s roughly 1.68 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 23,565 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. With an inclination of 55.8°, FREGAT R/B passes over latitudes between 55.8°N and 55.8°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 1,286 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 23,525 km (perigee) and 23,604 km (apogee), with an average altitude of approximately 23,565 km. It completes one orbit every 14 hours 19 minutes, travelling at approximately 13,136 km/h (8,163 mph).
FREGAT R/B (NORAD ID 41176) 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 2015-12-17 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 41176) 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 13,136 km/h (8,163 mph) — roughly 3.65 km/s. It completes 1.68 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.