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FREGAT R/B

NORAD 49811 Rocket Body MEO 2021-116C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
23515 km
Apogee
23572 km
Inclination
57.2°
Period
858.5 min
Mean Motion
1.67734451 rev/day
TLE Epoch
2026-06-24 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,544 km
Orbital Velocity13,141 km/h
Velocity3.65 km/s
Orbital Period14 hours 19 minutes
Orbits / Day1.68
Eccentricity0.0010
Semi-Major Axis29,915 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2021-12-05
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2021-116C
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 2021-12-05 from Guiana Space Centre, Kourou on the GalileoSat-27/28 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 23,515 km and 23,572 km with an inclination of 57.2°. It travels at approximately 13,141 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 23,544 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 57.2°, FREGAT R/B passes over latitudes between 57.2°N and 57.2°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 1,287 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 23,515 km (perigee) and 23,572 km (apogee), with an average altitude of approximately 23,544 km. It completes one orbit every 14 hours 19 minutes, travelling at approximately 13,141 km/h (8,165 mph).
FREGAT R/B (NORAD ID 49811) 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 2021-12-05 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 49811) 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 13,141 km/h (8,165 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.