Telstar 14 or Estrela do Sul 1 (Southern Star 1) is a commercial communications satellite in the Telstar series built by Space Systems/Loral (SS/L) for Telesat to provide Ku-band communications to South America and the Southern United States. Estrela do Sul 1 was launched by Sea Launch using a Zenit-3SL carrier rocket on 11 Jan 2004 for geosynchronous orbit at 63 degrees west.
Mission type | Communications |
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Operator | Loral Skynet (2004-07) Telesat (2007-11) |
COSPAR ID | 2004-001A ![]() |
SATCAT no. | 28137 |
Mission duration | 15 years planned |
Spacecraft properties | |
Bus | LS-1300 |
Manufacturer | Space Systems/Loral |
Launch mass | 4,695 kilograms (10,351 lb) |
Start of mission | |
Launch date | 11 January 2004, 04:12:59 (2004-01-11UTC04:12:59Z) UTC[1] |
Rocket | Zenit-3SL |
Launch site | Odyssey |
Contractor | Sea Launch |
End of mission | |
Disposal | Decommissioned |
Deactivated | c. 2011 (2012) |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 63° west |
Perigee altitude | 36,193 kilometres (22,489 mi) |
Apogee altitude | 36,207 kilometres (22,498 mi) |
Inclination | 1.95 degrees |
Period | 24.28 hours |
Epoch | 28 October 2013, 15:53:21 UTC[2] |
The North solar array failed to open after launch, limiting the mission effectiveness. The president of SS/L later said images of the satellite in orbit showed massive damage to the affected array, indicating that an explosion had occurred during launch.[3] The satellite entered service with reduced capacity (17 transponders) and reduced life span of 7 years with the jammed panel.[4]
Estrela do Sul 1 / Telstar 14 and Estrela do Sul 2 / Telstar 14R are built around the Loral 1300 satellite bus, and have launch mass of around 5000 kg.
The Telstar 14R replacement was launched in May 2011 from the Baikonur Cosmodrome in Kazakhstan aboard an International Launch Services Proton-M rocket. This replacement satellite, Telstar 14R experienced the same problem, with its north solar array failing to open. The Telstar 14R replacement satellite is in service, despite that deployment failure.[5]
← 2003 · Orbital launches in 2004 · 2005 → | |
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Estrela do Sul 1 | Progress M1-11 | AMC-10 | USA-176 | Molniya-1 No.93 | Rosetta (Philae) | MBSat | Eutelsat W3A | USA-177 | Globus No.17L | Superbird-A2 | Tansuo 1 · Naxing 1 | Soyuz TMA-4 | Gravity Probe B | Ekspress AM-11 | DirecTV-7S | AMC-11 | Formosat-2 | Progress M-49 | Kosmos 2405 | Kosmos 2406 | Intelsat 10-02 | USA-178 | Telstar 18 | Demeter · AprizeSat-1 · AprizeSat-2 · Saudisat-2 · SaudiComsat-1 · SaudiComsat-2 · UniSat-3 · AMSAT-Echo | Aura | Anik F2 | Kosmos 2407 | Tan Ce 2 | MESSENGER | Amazonas 1 | Progress M-50 | FSW-19 | USA-179 | Ofek-6 | Shijian 6A · Shijian 6B | GSAT-3 / EDUSAT | Kosmos 2408 · Kosmos 2409 | Kosmos 2410 | FSW-20 | Soyuz TMA-5 | AMC-15 | Feng Yun 2C | Ekspress AM-1 | Zi Yuan 2C | USA-180 | Tansuo 2 | Swift | AMC-16 | Helios IIA · Nanosat 01 · Essaim 1 · Essaim 2 · Essaim 3 · Essaim 4 · Parasol | HLVOLSDP · Sparkie · Ralphie | Progress M-51 | Sich-1M · MK-1TS | Kosmos 2411 · Kosmos 2412 · Kosmos 2413 | |
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. |