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Diadem
Diademe 1 Credit: Manufacturer Image |
French earth geodetic satellite. French geodetic satellites. Geodesy satellite for CNES, France. Launched 1967.
Status: Operational 1967. First Launch: 1967-02-08. Last Launch: 1967-02-15. Number: 2 . Gross mass: 23 kg (50 lb).
More at: Diadem.
Family:
Earth,
Earth geodetic sat.
Country:
France.
Launch Vehicles:
Diamant,
Diamant A.
Launch Sites:
Hammaguira,
Hammaguira Brigitte.
Agency:
CNES.
Bibliography:
2,
279,
6,
12225.
1967 February 8 - .
09:39 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
FAILURE: Partial Failure - injected into too low an orbit..
Failed Stage: 3.
- Diademe 1 - .
Payload: Diademe D-1C. Mass: 23 kg (50 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: Diadem.
USAF Sat Cat: 2674 . COSPAR: 1967-011A. Apogee: 1,084 km (673 mi). Perigee: 545 km (338 mi). Inclination: 40.00 deg. Period: 101.20 min. Orbit too low. Launch time of Diadem I was 10:39:40 on 8 Feb 1967. Launch time of Diadem II was 11:06:57 on 15 Feb 1967..
1967 February 15 - .
10:06 GMT - .
Launch Site:
Hammaguira.
Launch Complex:
Hammaguira Brigitte.
LV Family:
Diamant.
Launch Vehicle:
Diamant A.
- Diademe 2 - .
Payload: Diademe D-1D. Mass: 23 kg (50 lb). Nation: France.
Agency: CNES.
Class: Earth.
Type: Geodetic satellite. Spacecraft: Diadem.
USAF Sat Cat: 2680 . COSPAR: 1967-014A. Apogee: 1,733 km (1,076 mi). Perigee: 584 km (362 mi). Inclination: 39.40 deg. Period: 108.50 min. Launch time of Diadem I was 10:39:40 on 8 Feb 1967. Launch time of Diadem II was 11:06:57 on 15 Feb 1967. .
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