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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
Civil Geodetic
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
Cyl + 4 Pan, 0.8 m
Radar Cross Section
0.455 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 DIADEME 2
1 02680U 67014A   25258.28811122  .00000983  00000-0  42036-3 0  9999
2 02680  39.4418 241.7421 0703005 274.6097  77.4732 13.41116390839041
Epoch: 2025-09-15T06:54Z
TLE epoch observation values (Epoch: 2025-09-15T06:54:52.809Z)
Latitude
0.00002°
Longitude
143.52716°
Altitude
1,026.411 km
Speed
7.378 km/s
True Right ascension
16h 06m 58s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
14:12:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,633.71 km
Perigee altitude
581.226 km
Semi-major axis
7,485.605 km
Eccentricity
0.0703
Inclination
39.4418°
RAAN
241.7421°
Arg. of periapsis
274.6097°
True anomaly
85.46391°
Mean anomaly
77.4732°
Eccentric anomaly
81.45642°
Mean motion
3.35122 °/min
Orbital period
107.42 mins
BSTAR
0.00042036
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