Names | Superbird-6 |
---|---|
Mission type | Communications |
Operator | SKY Perfect JSAT Group |
COSPAR ID | 2004-011A [1] |
SATCAT no. | 28218 |
Website | Archived official page |
Mission duration | 13 years (planned) Failed on orbit (achieved) |
Spacecraft properties | |
Spacecraft | Superbird-6 |
Spacecraft type | Superbird |
Bus | BSS-601 |
Manufacturer | Boeing |
Launch mass | 3,100 kg (6,800 lb) |
BOL mass | 1,528 kg (3,369 lb) |
Dry mass | 1,477 kg (3,256 lb) |
Dimensions | 26.2 m × 7.5 m × 4.5 m (86 ft × 25 ft × 15 ft) with solar panels and antennas deployed |
Power | 4378 watts |
Start of mission | |
Launch date | 16 April 2004, 00:45:00 UTC[2] |
Rocket | Atlas IIAS |
Launch site | Cape Canaveral, LC-36B |
Contractor | International Launch Services (ILS) |
Entered service | Never in service |
End of mission | |
Disposal | Graveyard orbit |
Last contact | Failed on orbit |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Geostationary orbit |
Longitude | 158° East |
Transponders | |
Band | 23 Ku-band 36 MHz 4 Ka-band 100 MHz [4] |
Bandwidth | 1228 MHz |
Coverage area | Japan, South Asia, East Asia, Hawaii |
TWTA power | Ku-band: 85 watts Ka-band: 70 watts [4] |
Superbird-A2, known as Superbird-6 before launch, was a geostationary communications satellite ordered and operated by Space Communications Corporation (SCC) that was designed and manufactured by Hughes (now Boeing) on the BSS-601 satellite bus. It had a mixed Ku-band and Ka-band payload and was expected replace Superbird-A at the position at 158° East longitude. It was expected to provided television signals and business communications services throughout Japan, South Asia, East Asia, and Hawaii.[5][6][4]
While the launch was within the margins specified by the satellite manufacturer, the trajectory analysis had been inexact and the satellite suffered severe life and power degradation. It tried to use a supersynchronous transfer strategy, but Boeing had failed to take into consideration the effect of the Moon. Thus, the lowest part of the orbit dropped too fast and much propellant had to be spent on a fast transit to geosynchronous orbit. Additionally, the solar panels suffered damage from the extreme contact with the atmosphere. Given the damage to the spacecraft, it was never put into service.[5][7]
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