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FREGAT R/B

NORAD 63131 Rocket Body MEO 2025-042B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
19038 km
Apogee
19118 km
Inclination
65.1°
Period
673.7 min
Mean Motion
2.13754424 rev/day
TLE Epoch
2026-06-22 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,078 km
Orbital Velocity14,247 km/h
Velocity3.96 km/s
Orbital Period11 hours 14 minutes
Orbits / Day2.14
Eccentricity0.0016
Semi-Major Axis25,449 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2025-03-02
Launch Site
PKMTR
Int'l Designator
2025-042B
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 2025-03-02 from PKMTR on the Glonass-K2 No. 14L 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 19,038 km and 19,118 km with an inclination of 65.1°. It travels at approximately 14,247 km/h (3.96 km/s), completing one full orbit every 11 hours 14 minutes — that’s roughly 2.14 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 19,078 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 8 active payloads and 47 tracked debris or rocket body fragments — notable neighbours include COSMOS 1413 (GLONASS), COSMOS 1415 (GLONASS), COSMOS 1521 (GLONASS). This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 65.1°, FREGAT R/B passes over latitudes between 65.1°N and 65.1°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, of which 8 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 Medium Earth Orbit (MEO) at altitudes between 19,038 km (perigee) and 19,118 km (apogee), with an average altitude of approximately 19,078 km. It completes one orbit every 11 hours 14 minutes, travelling at approximately 14,247 km/h (8,853 mph).
FREGAT R/B (NORAD ID 63131) 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 2025-03-02 from PKMTR. View the full satellite launch log.
Yes — Orbital Radar tracks FREGAT R/B (NORAD ID 63131) 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 14,247 km/h (8,853 mph) — roughly 3.96 km/s. It completes 2.14 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.