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FREGAT R/B

NORAD 44553 Rocket Body MEO 2019-065B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2292 km
Apogee
37905 km
Inclination
63.3°
Period
714.6 min
Mean Motion
2.01516164 rev/day
TLE Epoch
2026-06-25 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,099 km
Orbital Velocity13,970 km/h
Velocity3.88 km/s
Orbital Period11 hours 55 minutes
Orbits / Day2.02
Eccentricity0.6727
Semi-Major Axis26,470 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2019-09-26
Launch Site
PKMTR
Int'l Designator
2019-065B
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 2019-09-26 from PKMTR on the EKS No. 3L? launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,292 km and 37,905 km with an inclination of 63.3°. It travels at approximately 13,970 km/h (3.88 km/s), completing one full orbit every 11 hours 55 minutes — that’s roughly 2.02 orbits per day. Its orbital eccentricity of 0.6727 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 20,099 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 5 active payloads and 20 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 63.3°, FREGAT R/B passes over latitudes between 63.3°N and 63.3°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 1,287 active satellites in total, of which 4 share a similar altitude band with FREGAT R/B.
🔗 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 2,292 km (perigee) and 37,905 km (apogee), with an average altitude of approximately 20,099 km. It completes one orbit every 11 hours 55 minutes, travelling at approximately 13,970 km/h (8,681 mph).
FREGAT R/B (NORAD ID 44553) 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 2019-09-26 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 44553) 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 13,970 km/h (8,681 mph) — roughly 3.88 km/s. It completes 2.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.