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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: 5 hours ago

TLE from 5 hours ago
0 DIADEME 2
1 02680U 67014A   25304.31334834  .00001977  00000-0  82475-3 0  9990
2 02680  39.4399  37.0300 0700831 177.1637 183.3377 13.41301063845224
Epoch: 2025-10-31T07:31Z
TLE epoch observation values (Epoch: 2025-10-31T07:31:13.296Z)
Latitude
Longitude
-115.63497°
Altitude
1,627.409 km
Speed
6.808 km/s
True Right ascension
02h 28m 07s
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
08:33:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,631.348 km
Perigee altitude
582.215 km
Semi-major axis
7,484.919 km
Eccentricity
0.07008
Inclination
39.4399°
RAAN
37.03°
Arg. of periapsis
177.1637°
True anomaly
182.90784°
Mean anomaly
183.3377°
Eccentric anomaly
183.1192°
Mean motion
3.35168 °/min
Orbital period
107.41 mins
BSTAR
0.00082475
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