Encyclopedia Astronautica
Malaysia


Malaysia

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Associated People
  • Muszaphar Muszaphar, Dr Sheikh (1972-) Malaysian physician cosmonaut. Flew on ISS EP-13. First Malaysian in space. More...
  • Khaleed bin Khaleed, Dr Faiz (1980-) Malaysian physician cosmonaut, 2006-2007. Backup to first Malaysian in space. More...

Associated Manufacturers and Agencies
  • BKSA Malaysian agency. Bahagian Kajian Sains Angkasa, Kuala Lumpur, Malaysia. More...

Associated Programs

Malaysia Chronology


1972 July 26 - .
  • Birth of Dr Sheikh Muszaphar - . Nation: Malaysia. Summary: Malaysian physician cosmonaut. Flew on ISS EP-13. First Malaysian in space..

1980 September 15 - .
  • Birth of Dr Faiz bin Khaleed - . Nation: Malaysia. Summary: Malaysian physician cosmonaut, 2006-2007. Backup to first Malaysian in space..

1996 January 12 - . 23:10 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V82.
  • Measat 1 - . Mass: 1,450 kg (3,190 lb). Nation: Malaysia. Agency: Binarian. Program: Measat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 23765 . COSPAR: 1996-002B. Apogee: 35,792 km (22,240 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geostationary at 91.4E. Positioned in geosynchronous orbit at 91 deg E in 1996-1999 As of 5 September 2001 located at 91.49 deg E drifting at 0.012 deg W per day. As of 2007 Mar 11 located at 91.50E drifting at 0.009W degrees per day..

1996 November 13 - . 22:40 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V92.
  • Measat 2 - . Nation: Malaysia. Agency: Binarian. Program: Measat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. USAF Sat Cat: 24653 . COSPAR: 1996-063B. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Geostationary at 148.0E. Positioned in geosynchronous orbit at 148 deg E in 1996-1999 As of 5 September 2001 located at 148.00 deg E drifting at 0.011 deg W per day. As of 2007 Mar 9 located at 147.98E drifting at 0.007W degrees per day..

2000 September 26 - . 10:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Tiungsat-1 - . Payload: MY-Sat 1. Mass: 50 kg (110 lb). Nation: Malaysia. Agency: BKSA. Manufacturer: Surrey. Class: Earth. Type: Earth resources satellite. Spacecraft: MicroSat-70. USAF Sat Cat: 26545 . COSPAR: 2000-057A. Apogee: 658 km (409 mi). Perigee: 644 km (400 mi). Inclination: 64.5585 deg. Period: 97.67 min. Launch delayed from August 25/26. Customer: Astonautic Technology (M) SDN. BHD. Malaysia's first microsatellite built through a technology transfer programme with Surrey Satellite Technology Ltd Carried multi-spectral Earth imaging CCD cameras, meteorological Earth imaging CCD camera, digital store and forward communications, cosmic-ray energy deposition experiment (CEDEX)

2006 December 11 - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz M. LV Configuration: Proton-M/Briz-M 535-21.
  • Measat 3 - . Mass: 4,900 kg (10,800 lb). Nation: Malaysia. Agency: Binarian. Program: Measat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 601. USAF Sat Cat: 29648 . COSPAR: 2006-056A. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Malaysian communications satellite, to be stationed at 91.5 East together with Measat 1, covering South Asia, Malaysia and Indonesia, and supplementing Measats 1 and 2 launched ten years earlier. The Proton booster released the satellite in a 416 x 35807 x 49.1 deg geosynchronous transfer orbit. The Boeing 601HP 3 axis stabilized spacecraft, had a design lifetime of 15 years. C-band 24 active transponders using 65-watt TWTAs; Ku-band 24 active transponders using 120-watt TWTAs . End of life power of 9.8 kW provided by two solar wings, each with 4 panels of triple-junction gallium arsenide solar cells. A 445N liquid apogee motor circularised the spacecraft in geosynchronous orbit, and 12 x 10 N bipropellant thrusters provided stabilization and stationkeeping. Length in orbit with solar panels deployed 26.2 m; width, with antennas deployed, 7.7 m; stowed diameter 3.8 m. Mass in geostationary orbit after apogee motor maneuver at beginning of life 3220 kg. As of 2007 Mar 11 located at 91.49E drifting at 0.012W degrees per day.

2009 June 21 - . 21:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC45/1. LV Family: Zenit. Launch Vehicle: Zenit-3SLB. LV Configuration: Zenit-3SLB s/n LL3.
  • Measat 3A - . Mass: 2,370 kg (5,220 lb). Nation: Malaysia. Agency: SIS. Program: Measat. Spacecraft: Star bus. USAF Sat Cat: 35362 . COSPAR: 2009-032A. Apogee: 35,788 km (22,237 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.00 min.

2009 July 14 - . 03:36 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein OM. LV Family: Falcon. Launch Vehicle: Falcon 1. LV Configuration: Falcon 1 s/n F1-5.
  • Razaksat - . Mass: 180 kg (390 lb). Nation: Malaysia. Agency: SpaceX. Spacecraft: Satrec. USAF Sat Cat: 35578 . COSPAR: 2009-037A. Apogee: 690 km (420 mi). Perigee: 665 km (413 mi). Inclination: 9.0000 deg. Period: 98.30 min. Summary: Malaysian imaging satellite..

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