Satélite Tecnológico (original) (raw)

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SATEC

Mission type Earth orbiter
Operator INPE
COSPAR ID F20030822A[1]
Mission duration 6 months (planned)
Spacecraft properties
Manufacturer INPE
Launch mass 65.0 kilograms (143.3 lb)
Start of mission
Launch date August 25, 2003 (2003-08-25Z) (planned)August 23, 2003, 16:30 UTC (Alcântara accident)
Rocket VLS-1 V3
Launch site Alcântara VLS Pad
Orbital parameters
Reference system Geocentric
Regime Heliosynchronous
Eccentricity 0
Perigee altitude 750 kilometres (470 mi)
Apogee altitude 750 kilometres (470 mi)
Inclination 15°
Period 100 minutes
Epoch Planned

The Satélite Tecnológico ("Technologic Satellite" in English) or SATEC, was a microsatellite of scientific applications, designed, developed, built and tested by Brazilian technicians, engineers and scientists working at INPE (National Institute for Space Research).

The primary objective of SATEC was to test the technological equipment embedded in the VLS-1, providing more information for future applications.

The SATEC scientific satellite had the following characteristics:

The instrumentation shipped in SATEC was as follows:

SATEC, which had an estimated life of 6 months, was lost with UNOSAT in the explosion of the VLS-1 launch vehicle on 23 August 2003 in an explosion three days before the launch date.[2][3] This event came to be known as Accident of Alcantara.

  1. ^ Wade, Mark. SATEC. Encyclopedia Astronautica. Retrieved 31 March 2017.
  2. ^ "UNOSAT 1". space.skyrocket.de. Retrieved 2020-06-04.
  3. ^ "SATEC". space.skyrocket.de. Retrieved 2020-06-04.