Official name OSCAR 23 (KITSAT 1)
Alternative name Uribyol 1
Cospar ID 1992-052B
Norad ID 22077
Launch date 1992-08-10
Launch site FRGUI
Launch vehicle Ariane-42P H10
Country/Organization South Korea
Type application Earth observation, technology
Operator Korean Institute of Technology (KIT)
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 111.93
Inclination (deg) 66.08
Perigee (km) 1303
Apogee (km) 1327
Eccentricity 0.0091254752851711
Mean motion (revs. per day) 12.8651835968909
Semi-Major axis (km) 7693.135
Raan (deg) 90.5544
Arg of perigee (deg) 281.2379
Shape Hex Poly
Mass (kg) 49.55
Height (m) 0.67
Width (m) 0.35
Depth (m) 0.67
Span (m^2) 0.67
Contractors SSTL (#1); KIT (#2)
Equipment see above
Propulsion None
Configuration Microsat-70
Power Solar cells, batteries

KITSAT-1 (Korean Institute of Technology Satellite) was a collaborative research mission, encompassing the installation of a groundstation in South Korea, participation of Korean engineers in the UoSAT-5 mission, technology transfer and training of students on the MSc courses at Surrey, and the involvement in a engineering and flight microsatellites.

KITSAT-1 was developed and constructed by a team of Korean and SSTL engineers. It was based on the 35 cm × 35 cm × 67 cm modular microsatellite bus previously flown on UoSAT-3, -4 and -5. Power was provided by body mountes solar cells. Attitude control was provided by a gravity-gradient boom and active magnetorquering.

The satellite payloads include:

  • Earth Imaging System (EIS)
    The EIS consists of two Charge Coupled Device (CCD) imagers, an optical system with two lenses and a Transputer Image Processor. One of the imagers provides a wide field of view with approximately 4 km ground resolution while the second operates in telephoto mode with 400 m ground resolution
  • Digital Signal Processing Experiment (DSPE)
    The DSPE comprises two Texas Instruments DSP microprocessors operating independently or in parallel. The purpose of the DSPE is to broadcast stored speech, relay compressed speech in real time, and implement advanced data link modulation techniques.
  • PACSAT Communications System (PCS)
    For Amateur Satellite service, the PCS provides digital Store and Forward communications for stations. The system uses standard protocols for message forwarding, with 9600 bps uplink and downlink rates. The PCS contains 13 MByte CMOS SRAM storage.
  • Cosmic Ray Experiment (CRE)
    The CRE is an experiment for radiation environment research and monitoring of its effects. It consists of a Total Dose Experiment (TDE) to measure total ionising dose, and a Cosmic Particle experiment (CPE) to monitor energetic particle events. The data collected from KITSAT-1's high altitude, inclined orbit were compared with that available from the UoSAT-3 and UoSAT-5 missions in 800 km polar orbits.

The follow on mission, KITSat 2 (Uribyol 2) was very similar, but flown in a different orbit. This time, the satellite was completely manufactured by the South Korean team at KIT.

KITSAT-2's payloads were:

  • KAIST Satellite Computer (KASCOM)
  • CCD Earth Imaging System (CEIS)
  • Digital Signal Processing Experiment (DSPE)
  • Low Energy Electron Detector (LEED)
  • Infrared Sensor Experiment (IREX)
  • Digital Store and Forward Communication Experiment (DSFCE)

The purpose of the KITSAT 2 mission was to improve and enhance the KITSAT-1 systems, to use domestically manufactured components, to demonstrate experimental modules and to promote domestic space industry.

Satellite COSPAR Date LS Launch Vehicle Remarks
OSCAR 23 (KITSAT 1) 1992-052B 1992-08-10 FRGUI Ariane-42P H10 with TOPEX Poseidon, S-80/T
KITSAT B 1993-061F 1993-09-26 FRGUI Ariane-40 H10 with SPOT 3, Stella, Healthsat 2, Eyesat 1, Itamsat, PoSAT 1