FREGAT R/B
NORAD 59073
Rocket Body
LEO
2024-039W
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LEO · NORAD 59073
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
708 km
Apogee
753 km
Inclination
89.0°
Period
99.4 min
Mean Motion
14.48628610 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude731 km
Orbital Velocity26,971 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.49
Eccentricity0.0032
Semi-Major Axis7,102 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2024-02-29
Launch Site
Vostochny, Russia
Int'l Designator
2024-039W
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 2024-02-29 from Vostochny, Russia on the Soyuz Rideshare 12 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 708 km and 753 km with an inclination of 89.0°. It travels at approximately 26,971 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.49 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. 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 731 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of FREGAT R/B’s average altitude, there are currently 359 active payloads and 1,862 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 89.0°, FREGAT R/B passes over latitudes between 89.0°N and 89.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,287 active satellites in total, of which 38 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 Low Earth Orbit (LEO) at altitudes between 708 km (perigee) and 753 km (apogee), with an average altitude of approximately 731 km. It completes one orbit every 99 minutes, travelling at approximately 26,971 km/h (16,759 mph).
FREGAT R/B (NORAD ID 59073) 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 2024-02-29 from Vostochny, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 59073) 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 26,971 km/h (16,759 mph) — roughly 7.49 km/s. It completes 14.49 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.