Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Melco
Japanese manufacturer of spacecraft. Melco, Japan.
AKA: Mitsubishi Denki Kabushiki-gaisha, Kamakura Works. Location: Kanagawa.
Country:
Japan.
Spacecraft:
Hinode.
2006 September 11 - .
04:35 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 202.
- IGS-3A - .
Mass: 850 kg (1,870 lb). Nation: Japan.
Agency: JIDF.
Manufacturer: Melco.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: IGS.
Decay Date: 2016-10-29 . USAF Sat Cat: 29393 . COSPAR: 2006-037A. Apogee: 491 km (305 mi). Perigee: 484 km (300 mi). Inclination: 97.30 deg. Information Gathering Satellite / Optical-2 military surveillance satellite, launched to replace IGS O-1 launched in 2003, which demonstrated technical problems. The first replacement, IGS-O-2, was lost in a launch failure in 2003..
2006 September 22 - .
21:36 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima M-V.
Launch Vehicle:
M-V.
- Hinode (Solar B) - .
Mass: 870 kg (1,910 lb). Nation: Japan.
Agency: JAXA.
Manufacturer: Melco.
Class: Astronomy.
Type: Solar satellite. Spacecraft: Hinode.
USAF Sat Cat: 29479 . COSPAR: 2006-041A. Apogee: 695 km (431 mi). Perigee: 674 km (418 mi). Inclination: 98.10 deg. Period: 98.50 min. Solar satellite with a large optical telescope and an X-ray telescope built by the Smithsonian Observatory..
2006 December 16 - .
06:32 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 204.
- Kiku 8 - .
Payload: ETS-8. Mass: 5,817 kg (12,824 lb). Nation: Japan.
Agency: JAXA.
Manufacturer: Melco.
Class: Technology.
Type: Navigation technology satellite. Spacecraft: DS2000.
USAF Sat Cat: 29656 . COSPAR: 2006-059A. Apogee: 35,798 km (22,243 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.0500 deg. Period: 1,436.11 min.
Engineering Test Satellite-8 was a Japanese prototype/operational demonstration for a number of new technologies: a large satellite bus, large-scale deployable 40-m-span antennae, mobile satellite communications system, mobile satellite digital multimedia broadcasting, and basic positioning using high-accuracy time standard devices. It will be positioned in geosynchronous orbit at 146 degrees East. JAXA developed two portable terrestrial systems to communicate directly with the satellite - a tiny telephone and a portable laptop computer. The satellite was to have a lifetime of ten years. As of 2007 Mar 11 located at 145.97E drifting at 0.010W degrees per day.
2007 February 24 - .
04:41 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima Y.
LV Family:
H-2.
Launch Vehicle:
H-IIA 2024.
- IGS 2 - .
Payload: IGS 4A. Mass: 1,200 kg (2,600 lb). Nation: Japan.
Agency: CSICE,
JAXA.
Manufacturer: Melco.
Class: Surveillance.
Type: Civilian Radarsat. Spacecraft: IGS.
Decay Date: 2014-04-13 . USAF Sat Cat: 30586 . COSPAR: 2007-005A. Information Gathering Satellite Radar-2. Japanese military satellite using a synthetic aperture radar for all-weather, 24-hour, high-resolution surveillance of the earth..
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use