DIADEME 2
Satellite information DIADEME 2
| Spacetrack Directory Name | DIADEME 2 |
| Follow DIADEME 2 | DIADEME 2 Tracker |
| Pass predictions DIADEME 2 | Pass predictions DIADEME 2 |
| Orbit launches |
1967-02-15 (59 years ago)
|
| Days in orbit | 21735 |
| Country/organisation of origin | Francja (FR) |
| Starting point | HGSTR (Hammaguir Launch Site, Algeria) |
| WWW | Here |
| Perigee | 578 km |
| Apogee | 1655 km |
| Orbit slope (inclination) | 39.44° |
| Laps per day | 13 |
| Height DIADEME 2 | 1123.27 km |
Additional information DIADEME 2
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.
satellite DIADEME 2 Date of exalting 15.02.1967y. Average height of ISS DIADEME 2 hundred 1123.27 km. Average velocity DIADEME 2 is 26255.29 km/h. Inclination DIADEME 2 satellite 39.44°.TLE
Average velocity DIADEME 2
Average inclination DIADEME 2
Mean right ascension of the ascending node (RAAN) DIADEME 2
Mean argument of perigee DIADEME 2
Mean semi-major axis of the orbit DIADEME 2
Mean orbital eccentricity DIADEME 2
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