DIAMANT DEB
NORAD 2684
Debris
LEO
1967-014C
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LEO · NORAD 2684
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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
545 km
Apogee
1176 km
Inclination
40.0°
Period
102.1 min
Mean Motion
14.09819715 rev/day
TLE Epoch
2026-09-20 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude861 km
Orbital Velocity26,727 km/h
Velocity7.42 km/s
Orbital Period102 minutes
Orbits / Day14.10
Eccentricity0.0436
Semi-Major Axis7,232 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1967-02-15
Launch Site
Hammaguir, Algeria
Int'l Designator
1967-014C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIAMANT DEB is a tracked piece of space debris attributed to France, launched on 1967-02-15 from Hammaguir, Algeria on the Diademe D-1D 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 545 km and 1,176 km with an inclination of 40.0°. It travels at approximately 26,727 km/h (7.42 km/s), completing one full orbit every 102 minutes — that’s roughly 14.10 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, DIAMANT DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
DIAMANT DEB orbits at an average altitude of 861 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 DEB’s average altitude, there are currently 282 active payloads and 2,140 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 40.0°, DIAMANT DEB 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 2 share a similar altitude band with DIAMANT DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
DIAMANT DEB orbits in Low Earth Orbit (LEO) at altitudes between 545 km (perigee) and 1,176 km (apogee), with an average altitude of approximately 861 km. It completes one orbit every 102 minutes, travelling at approximately 26,727 km/h (16,608 mph).
DIAMANT DEB (NORAD ID 2684) is a piece of tracked orbital debris attributed to France. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
DIAMANT DEB was launched on 1967-02-15 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 DEB (NORAD ID 2684) 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 DEB travels at approximately 26,727 km/h (16,608 mph) — roughly 7.42 km/s. It completes 14.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.42 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like DIAMANT DEB. Read more about debris statistics and the Kessler syndrome.