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DIAMANT R/B

NORAD 1805 Rocket Body LEO 1965-096B
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🛰️ Orbital Parameters
Perigee
509 km
Apogee
1360 km
Inclination
34.2°
Period
103.7 min
Mean Motion
13.88303115 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude935 km
Orbital Velocity26,592 km/h
Velocity7.39 km/s
Orbital Period104 minutes
Orbits / Day13.88
Eccentricity0.0582
Semi-Major Axis7,306 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1965-11-26
Launch Site
Hammaguir, Algeria
Int'l Designator
1965-096B
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 1965-11-26 from Hammaguir, Algeria on the A-1 launch. After more than 61 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 509 km and 1,360 km with an inclination of 34.2°. It travels at approximately 26,592 km/h (7.39 km/s), completing one full orbit every 104 minutes — that’s roughly 13.88 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 935 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DIAMANT R/B’s average altitude, there are currently 388 active payloads and 1,343 tracked debris or rocket body fragments. With an inclination of 34.2°, DIAMANT R/B passes over latitudes between 34.2°N and 34.2°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 2 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 509 km (perigee) and 1,360 km (apogee), with an average altitude of approximately 935 km. It completes one orbit every 104 minutes, travelling at approximately 26,592 km/h (16,523 mph).
DIAMANT R/B (NORAD ID 1805) 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 1965-11-26 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAMANT R/B (NORAD ID 1805) 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 26,592 km/h (16,523 mph) — roughly 7.39 km/s. It completes 13.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.