FREGAT R/B
NORAD 28923
Rocket Body
MEO
2005-051B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
23391 km
Apogee
23480 km
Inclination
59.0°
Period
853.9 min
Mean Motion
1.68647035 rev/day
TLE Epoch
2026-06-23 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,436 km
Orbital Velocity13,165 km/h
Velocity3.66 km/s
Orbital Period14 hours 14 minutes
Orbits / Day1.69
Eccentricity0.0015
Semi-Major Axis29,807 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2005-12-28
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2005-051B
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 2005-12-28 from Baikonur, Kazakhstan on the GSTB-v2/A launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 23,391 km and 23,480 km with an inclination of 59.0°. It travels at approximately 13,165 km/h (3.66 km/s), completing one full orbit every 14 hours 14 minutes — that’s roughly 1.69 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 23,436 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 6 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 59.0°, FREGAT R/B passes over latitudes between 59.0°N and 59.0°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 23,391 km (perigee) and 23,480 km (apogee), with an average altitude of approximately 23,436 km. It completes one orbit every 14 hours 14 minutes, travelling at approximately 13,165 km/h (8,180 mph).
FREGAT R/B (NORAD ID 28923) 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 2005-12-28 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 28923) 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 13,165 km/h (8,180 mph) — roughly 3.66 km/s. It completes 1.69 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.