JCSAT-1B, known as JCSAT-5 before launch, is a geostationary communications satellite operated by SKY Perfect JSAT Group (JSAT) which was designed and manufactured by Hughes (now Boeing) on the HS-601 satellite bus. It has a pure Ku-band payload and was used to replace JCSAT-1 at the 150° East longitude. It covers Japan, Korea, most of China, Thailand, Vietnam, Laos, part of Indonesia, part of Malaysia and Hawaii.[2][3][4]
Names | JCSAT-5 (Jun 1996 to Dec 1997) JCSAT-1B (Dec 1997 onward) |
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Mission type | Communications |
Operator | SKY Perfect JSAT Group |
COSPAR ID | 1997-075A [1] |
SATCAT no. | 25067 |
Website | http://www.jsat.net/en/contour/jcsat-1b.html |
Mission duration | 12 years (planned) |
Spacecraft properties | |
Spacecraft | JCSAT-5 |
Spacecraft type | JCSAT |
Bus | HS-601 |
Manufacturer | Hughes |
Launch mass | 2,982 kg (6,574 lb) |
Dry mass | 1,308 kg (2,884 lb) |
Dimensions | 26.1 m × 7.6 m (86 ft × 25 ft) with solar panels and antennas deployed |
Power | 5 kW |
Start of mission | |
Launch date | 2 December 1997, 22:52:32 UTC [1] |
Rocket | Ariane 44P |
Launch site | Centre Spatial Guyanais, ELA-2 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 150° East |
Transponders | |
Band | Ku-band: 16 × 36 Mhz + 16 × 27 Mhz |
Bandwidth | 1008 MHz |
Coverage area | Japan, East Asia, South Asia, Australia, Hawaii |
TWTA power | 12 × 36 Mhz 95 watts 4 × 36 Mhz 60 watts 16 × 27 Mhz 60 watts |
JCSAT constellation |
The spacecraft was designed and manufactured by Boeing Satellite Development Center on the HS-601 satellite bus. It had a launch mass of 2,982 kg (6,574 lb) and a 12-year design life. Its solar panels span 21 m (69 ft) when fully deployed and generated approximately 5 kW of power, with its antennas in fully extended configuration it is 7.6 m (25 ft) wide.[4] It would provide communications services throughout Japan, East Asia, South Asia, Australia and Hawaii.[2]
Its payload is composed of sixteen 36 MHz plus another sixteen 27 MHz Ku-band transponders, for a total bandwidth of 1008 MHz.[5] Its twelve of the 36 MHz transponders have a TWTA output power of 95 watts, the other four 36 MHz and the 27 MHz ones have 60 watts.[4][2] It can configure four 36 MHz transponders into two 76 MHz with an effective 95 watts.[2]
The Ku-band footprint covers Japan, Korea, most of China, Thailand, Vietnam, Laos, part of Indonesia, part of Malaysia and Hawaii.[4]
In June 1996, JSAT (since then merged into SKY Perfect JSAT Group) ordered JCSAT-5 from Hughes Space and Communications Company (now Boeing Satellite Development Center), to replace JCSAT-1 at the 150° East slot. The HS-601 based satellite would provide coverage to Japan, East Asia, Australia and Hawaii.[2]
An Ariane 44P successfully launched JCSAT-5 on 2 December 1997 at 22:52:32 UTC from Centre Spatial Guyanais ELA-2 launch pad. Once successfully deployed, it was renamed as JCSAT-1B. It was driven to the 150° East position where it replaced JCSAT-1.[2]
The satellite experienced an anomaly on 17 January 2007 on one of its thrusters. But after the operator designed a control scheme to handle the satellite without the failed thruster, it was put back into service.[2]
JCSAT satellites | |
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Launch designations | |
Operational designations |
← 1996 · Orbital launches in 1997 · 1998 → | |
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STS-81 | GPS IIR-1 | GE 2 · Nahuel 1A | Soyuz TM-25 | STS-82 | Haruka | Kosmos 2337 · Kosmos 2338 · Kosmos 2339 · Gonets-D1 #4 · Gonets-D1 #5 · Gonets-D1 #6 | JCSAT-R | USA-130 | Intelsat 801 | Mozhayets 2 | Tempo-2 | STS-83 | USA-131 | Progress M-34 | Kosmos 2340 | Thaicom 3 · BSAT-1a | Kosmos 2341 | Minisat 01 · Founders | GOES 10 | Iridium 4 · Iridium 5 · Iridium 6 · Iridium 7 · Iridium 8 | Chinasat 6A | Kosmos 2342 | STS-84 | Kosmos 2343 | Tselina-2 | Thor 2 | Telstar 5 | Inmarsat-3 F4 · INSAT-2D | Kosmos 2344 | Fengyun 2A | Iridium 9 · Iridium 10 · Iridium 11 · Iridium 12 · Iridium 13 · Iridium 14 · Iridium 16 | Intelsat 802 | STS-94 | Progress M-35 | Iridium 15 · Iridium 17 · Iridium 18 · Iridium 20 · Iridium 21 | USA-132 | Superbird-C | OrbView-2 | Soyuz TM-26 | STS-85 (CRISTA-SPAS) | PAS-6 | Kosmos 2345 | Agila 2 | Iridium 22 · Iridium 23 · Iridium 24 · Iridium 25 · Iridium 26 | Lewis | ACE | PAS-5 | FORTE | Iridium MFS-1 · Iridium MFS-2 | Hot Bird 3 · Meteosat 7 | GE-3 | Iridium 27 · Iridium 28 · Iridium 29 · Iridium 30 · Iridium 31 · Iridium 32 · Iridium 33 | Kosmos 2346 · FAISAT-2V | Intelsat 803 | Molniya-1T #98 | STS-86 | Iridium 19 · Iridium 34 · Iridium 35 · Iridium 36 · Iridium 37 | IRS-1D | Progress M-36 (Sputnik 40 · X-Mir) | EchoStar III | Foton #11 | Cassini (Huygens) | Apstar 2R | USA-133 | STEP-4 | USA-135 · FalconGOLD | Maqsat-B · Maqsat-H · YES | SCD-2A | USA-134 | USA-136 | Iridium 38 · Iridium 39 · Iridium 40 · Iridium 41 · Iridium 43 | Kupon | Sirius 2 · IndoStar-1 | Resurs-F1M #1 | STS-87 (SPARTAN-201) | TRMM · Orihime · Hikoboshi | JCSAT-1B · Equator-S | Astra 1G | Iridium 42 · Iridium 44 | Galaxy 8i | Kosmos 2347 | Kosmos 2348 | Progress M-37 | Iridium 45 · Iridium 46 · Iridium 47 · Iridium 48 · Iridium 49 | Intelsat 804 | Orbcomm FM5 · Orbcomm FM6 · Orbcomm FM7 · Orbcomm FM8 · Orbcomm FM9 · Orbcomm FM10 · Orbcomm FM11 · Orbcomm FM12 | Early Bird 1 | AsiaSat 3 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |