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). Payloads include a variety of satellites, spacecraft, and rockets 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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2680 intel report (Beta)
DIADEME 2 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | CNES |
| Mission | Civil Geodetic |
| Bus & Motor | D-1, Unknown motor |
| Mass | 23 kg wet, 23 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl + 4 Pan, 1.5 m |
| Radar Cross Section | 0.455 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 DIADEME 2
1 02680U 67014A 24355.30009629 .00000816 00000-0 35320-3 0 9993
2 02680 39.4418 357.4560 0708001 181.9226 177.8722 13.40528363802933Epoch: 2024-12-20T07:12Z
Definitive object data (Epoch: 2024-12-20T07:12:08.319Z)
| Latitude | -0.00001° |
| Longitude | 160.05374° |
| Altitude | 1,636.308 km |
| Speed | 6.801 km/s |
| True Right ascension | 23h 49m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -39.4301° |
| Longitude | 58.42932° |
| Altitude | 958.221 km |
| Speed | 7.452 km/s |
| Apparent Right ascension | 20h 13m 12s |
| Apparent Declination | -53° 44' 18" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:07:33 |
| Azimuth | 129.804° SE |
| Elevation | -48.924° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,639.793 km |
| Perigee altitude | 579.52 km |
| Semi-major axis | 7,487.793 km |
| Eccentricity | 0.0708001 |
| Inclination | 39.4418° |
| RAAN | 357.456° |
| Arg. of periapsis | 181.9226° |
| True anomaly | 178.14888° |
| Mean anomaly | 177.8722° |
| Eccentric anomaly | 178.01286° |
| Mean motion | 3.34975 °/min |
| BSTAR | 0.0003532 |
| Orbital period | 107.47 mins |
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Other satellites on launch #14 in the year 1967 (1967-02-15 UTC)
DIADEME 2 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2024-12-22 02:15:38.598Z | 202.541° SW | 2024-12-22 02:22:38.598Z | 151.822° SSE | 29.834° | 2024-12-22 02:30:38.598Z | 86.123° E |
| 15 mins | 2024-12-22 04:08:38.598Z | 241.087° WSW | 2024-12-22 04:16:38.598Z | 174.955° S | 42.93° | 2024-12-22 04:23:38.598Z | 82.529° E |
| 14 mins | 2024-12-22 06:03:38.598Z | 267.899° W | 2024-12-22 06:10:38.598Z | 253.087° W | 44.658° | 2024-12-22 06:17:38.598Z | 92.278° ESE |
| 11 mins | 2024-12-22 07:58:38.598Z | 277.267° WNW | 2024-12-22 08:04:38.598Z | 208.041° SW | 41.557° | 2024-12-22 08:09:38.598Z | 123.141° SE |
| 6 mins | 2024-12-22 09:54:38.598Z | 252.805° W | 2024-12-22 09:57:38.598Z | 215.818° SW | 19.327° | 2024-12-22 10:00:38.598Z | 177.803° S |
Authenticating...
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