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DIAMANT R/B

NORAD 2671 Rocket Body LEO 1967-011B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
538 km
Apogee
1011 km
Inclination
40.0°
Period
100.3 min
Mean Motion
14.35133581 rev/day
TLE Epoch
2026-09-15 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude775 km
Orbital Velocity26,888 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.35
Eccentricity0.0331
Semi-Major Axis7,146 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1967-02-08
Launch Site
Hammaguir, Algeria
Int'l Designator
1967-011B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DIAMANT R/B is a spent rocket body associated with France, launched on 1967-02-08 from Hammaguir, Algeria on the Diademe D-1C launch. After more than 59 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 538 km and 1,011 km with an inclination of 40.0°. It travels at approximately 26,888 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.35 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like DIAMANT 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
DIAMANT R/B orbits at an average altitude of 775 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 DIAMANT R/B’s average altitude, there are currently 444 active payloads and 2,331 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0455. With an inclination of 40.0°, DIAMANT R/B passes over latitudes between 40.0°N and 40.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. France operates approximately 124 active satellites in total, of which 3 share a similar altitude band with DIAMANT 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
DIAMANT R/B orbits in Low Earth Orbit (LEO) at altitudes between 538 km (perigee) and 1,011 km (apogee), with an average altitude of approximately 775 km. It completes one orbit every 100 minutes, travelling at approximately 26,888 km/h (16,707 mph).
DIAMANT R/B (NORAD ID 2671) is a spent rocket body — the upper stage of a launch vehicle attributed to France. 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.
DIAMANT R/B was launched on 1967-02-08 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAMANT R/B (NORAD ID 2671) 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.
DIAMANT R/B travels at approximately 26,888 km/h (16,707 mph) — roughly 7.47 km/s. It completes 14.35 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.