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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: 6 hours ago

TLE from 6 hours ago
0 DIADEME 2
1  2680U 67014A   26043.77484436  .00001388  00000-0  59506-3 0  9990
2  2680  39.4375 292.2039 0698981  53.0394 313.2291 13.41717098859252
Epoch: 2026-02-12T18:35Z
TLE epoch observation values (Epoch: 2026-02-12T18:35:46.552Z)
Latitude
-0.00002°
Longitude
-129.56186°
Altitude
765.055 km
Speed
7.64 km/s
True Right ascension
19h 28m 48s
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
03:33:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.309 km
Perigee altitude
582.162 km
Semi-major axis
7,483.373 km
Eccentricity
0.0699
Inclination
39.4375°
RAAN
292.2039°
Arg. of periapsis
53.0394°
True anomaly
307.03476°
Mean anomaly
313.2291°
Eccentric anomaly
310.16879°
Mean motion
3.35272 °/min
Orbital period
107.38 mins
BSTAR
0.00059506
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