From Wikipedia, the free encyclopedia
Formosat-1
(福爾摩沙衛星一號, formerly known as
ROCSAT-1
) was an
Earth observation satellite
operated by the National Space Program Office (NSPO, now the
National Space Organization
) of the
Republic of China
(
Taiwan
) to conduct observations of the
ionosphere
and
oceans
. The spacecraft and its instrumentation were developed jointly by NSPO and
TRW
using TRW's
Lightsat
bus, and was launched from
Cape Canaveral Air Force Station
,
US
, by
Lockheed Martin
on January 27, 1999.
[2]
FormoSat-1 provided 5½ years of operational service. The spacecraft ended its mission on June 17, 2004 and was decommissioned on July 16, 2004.
[3]
[4]
Technical details
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Spacecraft
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- Weight: 401 kg
- Shape: Hexagonal
- Dimensions
- Height: 2.1 m
- Diameter: 1.1 m
- Solar arrays: Two, 1.16 x 2.46 m
- Electrical power: 450 watts
Instrumentation
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- Experimental Communication Payload (ECP)
- Ionosphere Plasma Electrodynamics Instrument (IPEI)
- Ocean Color Imager (OCI)
Orbit
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- Altitude: 600 km
- Type: Circular
- Inclination: 35 degrees
See also
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References
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External links
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Launches are separated by dots ( ? ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights
are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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