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FREGAT R/B

NORAD 100745 Rocket Body MEO 2026-216B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
19150 km
Apogee
19442 km
Inclination
64.8°
Period
682.3 min
Mean Motion
2.11036950 rev/day
TLE Epoch
2026-09-17 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,296 km
Orbital Velocity14,187 km/h
Velocity3.94 km/s
Orbital Period11 hours 22 minutes
Orbits / Day2.11
Eccentricity0.0057
Semi-Major Axis25,667 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2026-09-17
Launch Site
Plesetsk Cosmodrome, Russia
Int'l Designator
2026-216B
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
FREGAT R/B is a spent rocket body associated with Russia (CIS), launched on 2026-09-17 from Plesetsk Cosmodrome, Russia on the Glonass launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 19,150 km and 19,442 km with an inclination of 64.8°. It travels at approximately 14,187 km/h (3.94 km/s), completing one full orbit every 11 hours 22 minutes — that’s roughly 2.11 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 19,296 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 9 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 64.8°, FREGAT R/B passes over latitudes between 64.8°N and 64.8°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 1,536 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 19,150 km (perigee) and 19,442 km (apogee), with an average altitude of approximately 19,296 km. It completes one orbit every 11 hours 22 minutes, travelling at approximately 14,187 km/h (8,815 mph).
FREGAT R/B (NORAD ID 100745) 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 2026-09-17 from Plesetsk Cosmodrome, Russia, Russia’s northern military cosmodrome, used primarily for high-inclination and polar orbit launches. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 100745) 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 14,187 km/h (8,815 mph) — roughly 3.94 km/s. It completes 2.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.