FREGAT R/B
NORAD 44300
Rocket Body
MEO
2019-030B
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
19284 km
Apogee
19637 km
Inclination
64.3°
Period
688.9 min
Mean Motion
2.09028740 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,461 km
Orbital Velocity14,142 km/h
Velocity3.93 km/s
Orbital Period11 hours 29 minutes
Orbits / Day2.09
Eccentricity0.0068
Semi-Major Axis25,832 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2019-05-27
Launch Site
PKMTR
Int'l Designator
2019-030B
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 2019-05-27 from PKMTR on the Uragan-M No. 758 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 19,284 km and 19,637 km with an inclination of 64.3°. It travels at approximately 14,142 km/h (3.93 km/s), completing one full orbit every 11 hours 29 minutes — that’s roughly 2.09 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 19,461 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 64.3°, FREGAT R/B passes over latitudes between 64.3°N and 64.3°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 19,284 km (perigee) and 19,637 km (apogee), with an average altitude of approximately 19,461 km. It completes one orbit every 11 hours 29 minutes, travelling at approximately 14,142 km/h (8,787 mph).
FREGAT R/B (NORAD ID 44300) 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 2019-05-27 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 44300) 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 14,142 km/h (8,787 mph) — roughly 3.93 km/s. It completes 2.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.