• Khaleed. - Dr Faiz bin Khaleed Malaysian Physician Cosmonaut. Born 15 September 1980.

• Muszaphar. - Dr Sheikh Muszaphar Shukor Al Masrie Malaysian Physician Cosmonaut. Born 26 July 1972. Number of Flights: 1.00. Total Time: 10.88 days.

1996 January 12 - 23:10 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44L. LV Configuration: Ariane 44L V82.

• Measat 1 Program: Measat. Mass: 1,450 kg (3,190 lb). Class: Communications. Spacecraft: HS 376. Agency: Binarian. Perigee: 35,783 km (22,234 mi). Apogee: 35,792 km (22,240 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1996-002B. USAF Sat Cat: 23765. 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. References: 2, 6. Level: 1.

• Measat 2 Program: Measat. Class: Communications. Spacecraft: HS 376. Agency: Binarian. Perigee: 35,781 km (22,233 mi). Apogee: 35,792 km (22,240 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1996-063B. USAF Sat Cat: 24653. 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. References: 2. Level: 1.

• Tiungsat-1 Payload: MY-Sat 1. Mass: 50 kg (110 lb). Class: Earth. Type: Landsat. Spacecraft: MicroSat-70. Manufacturer: Surrey/ATSB. Agency: BKSA. Perigee: 644 km (400 mi). Apogee: 658 km (409 mi). Inclination: 64.56 deg. Period: 97.67 min. COSPAR: 2000-057A. USAF Sat Cat: 26545. 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) References: 2, 552, 554. Level: 1.

• Measat 3 Program: Measat. Mass: 4,900 kg (10,800 lb). Class: Communications. Spacecraft: HS 601. Agency: Binarian. Perigee: 35,782 km (22,233 mi). Apogee: 35,792 km (22,240 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2006-056A. USAF Sat Cat: 29648. 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. References: 2. Level: 1.