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FREGAT R/B

NORAD 39621 Rocket Body MEO 2014-012B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
19300 km
Apogee
19638 km
Inclination
65.4°
Period
689.3 min
Mean Motion
2.08922210 rev/day
TLE Epoch
2026-06-24 08:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,469 km
Orbital Velocity14,139 km/h
Velocity3.93 km/s
Orbital Period11 hours 29 minutes
Orbits / Day2.09
Eccentricity0.0065
Semi-Major Axis25,840 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2014-03-23
Launch Site
PKMTR
Int'l Designator
2014-012B
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 2014-03-23 from PKMTR on the Uragan-M No. 754 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 19,300 km and 19,638 km with an inclination of 65.4°. It travels at approximately 14,139 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 19,469 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 65.4°, FREGAT R/B passes over latitudes between 65.4°N and 65.4°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 19,300 km (perigee) and 19,638 km (apogee), with an average altitude of approximately 19,469 km. It completes one orbit every 11 hours 29 minutes, travelling at approximately 14,139 km/h (8,786 mph).
FREGAT R/B (NORAD ID 39621) 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 2014-03-23 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 39621) 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 14,139 km/h (8,786 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.