Star One D1
Names | Hispasat 84W-2 H84W-2 [1] |
---|---|
Mission type | Communications |
Operator | Embratel |
COSPAR ID | 2016-082B ![]() |
SATCAT no. | 41904 |
Website | https://www.embratel.com.br/ |
Mission duration | 15 years (planned) 7 years, 7 months and 20 days (in progress) |
Spacecraft properties | |
Spacecraft | Star One D1 |
Bus | SSL 1300E |
Manufacturer | Space Systems/Loral |
Launch mass | 6,443 kg (14,204 lb) |
Power | 16 kW |
Start of mission | |
Launch date | 21 December 2016, 20:30 UTC |
Rocket | Ariane 5 ECA |
Launch site | Centre Spatial Guyanais, ELA-3 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 84° West |
Transponders | |
Band | 70 transponders: 28 C-band 24 Ku-band 18 Ka-band |
Coverage area | Brazil, Latin America |
Star One constellation ← Star One C4 Star One D2 → |
Star One D1 is a communications satellite operated by Embratel Star One with headquarters in Rio de Janeiro, Brazil. It was built by Space Systems/Loral (SSL) based on the SSL 1300 satellite bus. The satellite was successfully launched into space on 21 December 2016 at 20:30 UTC with an Ariane 5 ECA launch vehicle from the Centre Spatial Guyanais in French Guiana, together with the JCSAT-15. It had a launch mass of 6,340 kg (13,980 lb).[2]
Coverage
Star One D1 is equipped with 28 C-band transponders, 24 Ku-band transponders, and 18 Ka-Band transponders to meet the data, audio, video, and Internet demands of corporate and enterprise customers in Brazil, and Latin America.[1]
In addition, the Star One D1 satellite is capable of being used by large companies and government institutions. The satellite is capable of receiving and transmitting television, radio, telephony, internet, and other data signals for entertainment, telemedicine, tele-education and business applications, necessary for the interconnection of the Latin Americans countries and essential for the most distant communities.[3]
See also
- Star One (satellite operator)
- Star One C2
- Star One C3
- Star One C12
References
External links
- Embratel Archived 3 October 2013 at the Wayback Machine
- Satbeams
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- BeiDou M3-S
- USA-266 / GPS IIF-12
- Kosmos 2514 / GLONASS-M 751
- Kwangmyŏngsŏng-4
- USA-267 / Topaz-4
- Sentinel-3A
- ASTRO-H / Hitomi
- SES-9
- Eutelsat 65 West A
- IRNSS-1F
- Resurs-P №3
- ExoMars Trace Gas Orbiter, Schiaparelli EDM
- Soyuz TMA-20M
- Cygnus CRS OA-6 (Diwata-1, Flock-2e' × 20 , Lemur-2 × 9)
- Kosmos 2515 / Bars-M 2L
- BeiDou IGSO-6
- Progress MS-02
- Shijian-10
- Dragon CRS-8, BEAM
- Sentinel-1B, MICROSCOPE, e-st@r-II
- Mikhailo Lomonosov
- IRNSS-1G
- JCSAT-14
- Yaogan 30
- Galileo FOC-10, FOC-11
- Thaicom 8
- Kosmos 2516 / GLONASS-M 753
- Ziyuan III-02, ÑuSat 1, 2
- Kosmos 2517 / Geo-IK-2 №12
- Intelsat 31 / DLA-2
- USA-268 / Orion 9
- BeiDou G7
- Eutelsat 117 West B, ABS-2A
- Cartosat-2C, M3MSat, Flock-2p × 12, SathyabamaSat, Swayam
- MUOS-5
- Chinese next-generation crew capsule scale model
- Shijian 16-02
- Soyuz MS-01
- Progress MS-03
- Dragon CRS-9
- USA-269 / NROL-61
- AMOS-6†
- INSAT-3DR
- OSIRIS-REx
- Ofek-11
- Tiangong-2
- SkySat × 4
- ScatSat-1, Alsat-1B, Alsat-2B, BlackSky Pathfinder-1, Pratham, CanX-7, PISat
- Himawari 9
- Shijian-17
- XPNAV 1
- WorldView-4, CELTEE 1, Prometheus-2 × 2, AeroCube 8 × 2, U2U, RAVAN
- Yunhai-1
- Galileo FOC 7, 12, 13, 14
- Soyuz MS-03
- GOES-R
- Tianlian I-04
- Progress MS-04
- Göktürk-1
- Resourcesat-2A
- WGS-8
- HTV-6 / Kounotori 6, (EGG, TuPOD, UBAKUSAT, AOBA-VELOX, STARS, FREEDOM, ITF, Waseda-SAT, OSNSAT, Tancredo-1, TechEDSat, Lemur-2 × 4)
- Fengyun 4A
- CYGNSS × 8
- EchoStar 19
- Arase / ERG
- TanSat, Spark × 2
- Star One D1, JCSAT-15
- SuperView / Gaojing-1 01, 02, Bayi Kepu 1
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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