FREGAT R/B
NORAD 43235
Rocket Body
MEO
2018-024E
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MEO · NORAD 43235
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🛰️ Orbital Parameters
Perigee
7656 km
Apogee
7686 km
Inclination
0.0°
Period
276.2 min
Mean Motion
5.21348135 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,671 km
Orbital Velocity19,180 km/h
Velocity5.33 km/s
Orbital Period4 hours 36 minutes
Orbits / Day5.21
Eccentricity0.0011
Semi-Major Axis14,042 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2018-03-09
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2018-024E
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 2018-03-09 from Guiana Space Centre, Kourou on the O3b FM13/14/15/16 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 7,656 km and 7,686 km with an inclination of 0.0°. It travels at approximately 19,180 km/h (5.33 km/s), completing one full orbit every 4 hours 36 minutes — that’s roughly 5.21 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 7,671 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 0 active payloads and 11 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 0.0°, FREGAT R/B passes over latitudes between 0.0°N and 0.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 7,656 km (perigee) and 7,686 km (apogee), with an average altitude of approximately 7,671 km. It completes one orbit every 4 hours 36 minutes, travelling at approximately 19,180 km/h (11,918 mph).
FREGAT R/B (NORAD ID 43235) 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 2018-03-09 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 43235) 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 19,180 km/h (11,918 mph) — roughly 5.33 km/s. It completes 5.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 10 sunrises and sunsets every 24 hours.