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Launch Schedules

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   ROCSAT 2 - Summary
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The primary objective of the ROCSAT 2 (ROC Satellite No. 2) satellite mission is to observe and monitor the terrestrial and marine environment and natural resources throughout Taiwan, its remote islands and surrounding ocean for civil applications. In addition, the ROCSAT 2 satellite also carries a 'Sprites Imager' scientific instrument to study the electrodynamical coupling between thunderclouds and the upper atmosphere by taking images of lightening discharges.

The 700 kg (1543 lbm) satellite will be placed in a 890 km (480 nmi) sun-synchronous orbit with a 98.99 degree inclination. It is planned for a 5 year mission.

The US$75 million (2.37 billion Taiwan dollars) ROCSAT 2 program was approved in Oct 1997. NPSO has signed a contract with France's Matra Marconi Space on November 29, 1999, to build the ROCSAT 2 satellite, after canceling a contract with a German consortium because of pressure from mainland China. Matra Marconi Space is responsible for the satellite's payload and bus, with the rest of the project to be completed by six Taiwanese companies, including Acer, Tatung, Shihlin Electric & Engineering and Tay Yung Engineering Co. to supply components such as flight software, S-band antennae and other computer equipment for the project. ROCSAT 2 will be the first application for Matra Marconi’s standard small satellite bus, Leostar. Matra Marconi Space was the losing bidder in the original round, and has been able to secure French government approval for an export sale.

DaimlerChrysler Aerospace’s Dornier Satelliten unit had won a bid to build ROCSAT 2 for Taiwan's National Space Program February 8, 1999. However, the company was forced to back out of the contract on November 5, 1999, when the German government refused to grant an export permit for satellite-related technology to Taiwan. The US$600,000 deposit was returned to the Taiwanese government. Matra Marconi Space and Dornier Satelliten are now both of Astrium.

 

ROCSAT 2
Republic of China Satellite No. 2

SATELLITE

Int'l Designation  

Scheduled

Owner / Sponsor NPSO (Taiwan) / National Space Program Office
Mission Observation 
Satellite bus Astrium (Matra Marconi Space)

LEOSTAR

Launch Mass 700 kg (1543 lbm) 
Dimensions, stowed  
Mission Orbit SSO / 890 km (480 nmi)

98.99°

Design Life 5 years
Power (EOL)  

LAUNCH

Launch Vehicle Model Taurus
Date / Time (UTC) 2003  

FINANCIAL

Satellite cost US$75 million (2.37 billion Taiwan dollars) 
Web Links  

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