DIADEME 2
NORAD 2680
Payload
LEO
1967-014A
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LEO · NORAD 2680
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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
577 km
Apogee
1625 km
Inclination
39.4°
Period
107.3 min
Mean Motion
13.42262500 rev/day
TLE Epoch
2026-10-21 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,101 km
Orbital Velocity26,294 km/h
Velocity7.30 km/s
Orbital Period107 minutes
Orbits / Day13.42
Eccentricity0.0701
Semi-Major Axis7,472 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇫🇷 CNES (France)
Launch Date
1967-02-15
Launch Site
Hammaguir, Algeria
Int'l Designator
1967-014A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIADEME 2 is an active satellite operated by CNES (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 577 km and 1,625 km with an inclination of 39.4°. It travels at approximately 26,294 km/h (7.30 km/s), completing one full orbit every 107 minutes — that’s roughly 13.42 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks DIADEME 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DIADEME 2 orbits at an average altitude of 1,101 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 DIADEME 2’s average altitude, there are currently 437 active payloads and 504 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 39.4°, DIADEME 2 passes over latitudes between 39.4°N and 39.4°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 DIADEME 2.
❓ Frequently Asked Questions
DIADEME 2 orbits in Low Earth Orbit (LEO) at altitudes between 577 km (perigee) and 1,625 km (apogee), with an average altitude of approximately 1,101 km. It completes one orbit every 107 minutes, travelling at approximately 26,294 km/h (16,338 mph).
DIADEME 2 is operated by CNES (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2680. You can track DIADEME 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DIADEME 2 was launched on 1967-02-15 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIADEME 2 (NORAD ID 2680) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
DIADEME 2 travels at approximately 26,294 km/h (16,338 mph) — roughly 7.30 km/s. It completes 13.42 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.