TiungSat-1

TiungSat-1
Tiung Sat-1
Fecha de lanzamiento 26 de septiembre de 2000
Vehículo de lanzamiento Dnepr-1
Sitio de lanzamiento Baikonur
Masa 50 kg
NSSDC ID 2000-057D
Elementos orbitales
Tipo de órbita OTB
Inclinación 65°
Período orbital 97'
Apoastro 737 km
Periastro 522 km

El TiungSat-1 es el primer micro-satélite malasio.[1] Fue desarrollado a través de la colaboración y transferencia tecnológica entre Astronautic Technology Sdn Bhd (Malasia) y la Surrey Satellite Technology Ltd (Reino Unido). El satélite fue lanzado el 26 de septiembre de 2000 a bordo de un cohete Dnepr-1 desde el Cosmódromo de Baikonur (Kazajistán).[2]

Referencias

  1. TiungSat
  2. «Third satellite launch this year for SSTL: TiungSAT-1 in orbit» (en inglés). Surrey Satellite Technology Ltd (27 de septiembre de 2000). Consultado el 5-8-2009.

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