Nexus (FO-99, Fuji-OSCAR 99)

Launch data: Designation  43937 / 19003F Launch date  18 Jan 2019 - 00:50 UT Launch site  Uchinoura, LP-M Launch vehicle  Epsilon CLPS Mission  Technology, Amateur radio Earth orbit: Perigee / Apogee  480 x 512 km Eccentricity   Inclination  97.3° Period   min

Spacecraft data: Prime manufacturer  Nihon University, JAMSAT Platform  CubeSat 1U Operator  Nihon University, JAMSAT Mass at launch  1.3 kg Dry Mass   kg Basic shape   Dimension (m)   Equipment   Solar array  Solar cells Stabilization   Propulsion   DC power   Design lifetime

Description:

• Nexus is a 1U cubesat from Nihon University with an amateur radio payload.
• The NEXUS(NExt generation X Unique Satellite: NEXUS)is the forth satellite of Nihon University. The size is 1 U, mass is about 1.3 kg, and it is characterized by having 4 antennas. The main mission of "NEXUS" is "demonstration of next generation amateur satellite communication technology". We will do various missions such as operation of a p / 4 shift QPSK transmitter capable of high speed and low transmission power communication, a FSK transmitter with variable transmission speed, and analog data relay using a linear transponder.
• Specfications:
  

External links:

• Nihon University: Satellite Information
• Satellite tracking (n2ya.com): Real time satellite tracking