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DIADEME 2, 2680

Orbit data source: Space-Track

DIADEME 2, 2680 is a payload satellite owned by CNES (FR) in LEO that was launched on Wed, 15 Feb 1967 UTC via a DIAMANT A launch vehicle from the Hamma Guira Space Track Range (HGSTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
2680, 1967-014A
Orbit
LEO
Country
Flag of FRFR
Related business
Manufacturer
CNES
Mission
Spacecraft
Bus & Motor
D-1, Unknown motor
Mass
23 kg wet, 23 kg dry
Launch date (UTC)
1967-02-15 (59 years ago)
Launch vehicle
DIAMANT A
Launch site
Hamma Guira Space Track Range (HGSTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 DIADEME 2
1  2680U 67014A   26133.54205157  .00000736  00000-0  31979-3 0  9996
2  2680  39.4405 252.5111 0700062 205.5910 150.8542 13.41980679871310
Epoch: 2026-05-13T13:00Z
TLE epoch observation values (Epoch: 2026-05-13T13:00:33.255Z)
Latitude
-0.00004°
Longitude
-173.92809°
Altitude
1,566.552 km
Speed
6.863 km/s
True Right ascension
16h 50m 02s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
09:18:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.07 km
Perigee altitude
580.442 km
Semi-major axis
7,482.393 km
Eccentricity
0.07001
Inclination
39.4405°
RAAN
252.5111°
Arg. of periapsis
205.591°
True anomaly
154.48074°
Mean anomaly
150.8542°
Eccentric anomaly
152.69423°
Mean motion
3.35338 °/min
Orbital period
107.35 mins
BSTAR
0.00031979
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