DIAMANT R/B
NORAD 2017
Rocket Body
MEO
1966-013B
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MEO · NORAD 2017
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
495 km
Apogee
2078 km
Inclination
34.1°
Period
111.3 min
Mean Motion
12.93788015 rev/day
TLE Epoch
2026-09-15 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,287 km
Orbital Velocity25,973 km/h
Velocity7.21 km/s
Orbital Period111 minutes
Orbits / Day12.94
Eccentricity0.1034
Semi-Major Axis7,658 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1966-02-17
Launch Site
Hammaguir, Algeria
Int'l Designator
1966-013B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIAMANT R/B is a spent rocket body associated with France, launched on 1966-02-17 from Hammaguir, Algeria on the Diapason D-1A launch. After more than 60 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 495 km and 2,078 km with an inclination of 34.1°. It travels at approximately 25,973 km/h (7.21 km/s), completing one full orbit every 111 minutes — that’s roughly 12.94 orbits per day. Its orbital eccentricity of 0.1034 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,287 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 DIAMANT R/B’s average altitude, there are currently 22 active payloads and 388 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 34.1°, DIAMANT R/B passes over latitudes between 34.1°N and 34.1°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 Medium Earth Orbit (MEO) at altitudes between 495 km (perigee) and 2,078 km (apogee), with an average altitude of approximately 1,287 km. It completes one orbit every 111 minutes, travelling at approximately 25,973 km/h (16,139 mph).
DIAMANT R/B (NORAD ID 2017) 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 1966-02-17 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAMANT R/B (NORAD ID 2017) 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 25,973 km/h (16,139 mph) — roughly 7.21 km/s. It completes 12.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.