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FREGAT R/B

NORAD 47720 Rocket Body HEO 2021-016B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
537 km
Apogee
40109 km
Inclination
63.3°
Period
723.7 min
Mean Motion
1.98977411 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,323 km
Orbital Velocity13,911 km/h
Velocity3.86 km/s
Orbital Period12 hours 4 minutes
Orbits / Day1.99
Eccentricity0.7412
Semi-Major Axis26,694 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2021-02-28
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2021-016B
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 2021-02-28 from Baikonur, Kazakhstan on the Arktika-M No. 1 launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 537 km and 40,109 km with an inclination of 63.3°. It travels at approximately 13,911 km/h (3.86 km/s), completing one full orbit every 12 hours 4 minutes — that’s roughly 1.99 orbits per day. Its orbital eccentricity of 0.7412 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 follows a Highly Elliptical Orbit, sweeping between 537 km (perigee) and 40,109 km (apogee). It spends most of its 12 hours 4 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of FREGAT R/B’s average altitude, there are currently 0 active payloads and 12 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 1,286 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 follows a Highly Elliptical Orbit, swinging between 537 km (perigee) and 40,109 km (apogee). It spends most of its 12 hours 4 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
FREGAT R/B (NORAD ID 47720) 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 2021-02-28 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 47720) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,911 km/h (3.86 km/s), completing one revolution every 12 hours 4 minutes. Learn more about highly elliptical orbits.