Showing default

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.

Loading next visibility...
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: 1 day ago

TLE from 1 day ago
0 DIADEME 2
1 02680U 67014A   26089.03145048  .00001631  00000-0  67763-3 0  9997
2 02680  39.4409  90.7198 0700292 311.3458  42.9025 13.41861983865337
Epoch: 2026-03-30T00:45Z
TLE epoch observation values (Epoch: 2026-03-30T00:45:17.321Z)
Latitude
-0.00001°
Longitude
-108.0312°
Altitude
736.496 km
Speed
7.669 km/s
True Right ascension
06h 02m 52s
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
06:50:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,628.714 km
Perigee altitude
580.68 km
Semi-major axis
7,482.834 km
Eccentricity
0.07003
Inclination
39.4409°
RAAN
90.7198°
Arg. of periapsis
311.3458°
True anomaly
48.72842°
Mean anomaly
42.9025°
Eccentric anomaly
45.77794°
Mean motion
3.35308 °/min
Orbital period
107.36 mins
BSTAR
0.00067763
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|