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BEGIN:VEVENT
SUMMARY:(NET) Electron • PRELUDE & OrigamiSat 2
DTSTART;VALUE=DATE:20260101
DTEND;VALUE=DATE:20260102
UID:166975884380
DESCRIPTION:A Rocket Lab Electron rocket will launch 8 CubeSats for JAXA w
 hich were originally planned to launch together with the RAISE 4 satellite
  on an Epsilon S rocket. The payloads are PRELUDE\, OrigamiSat 2\, Mono-Ni
 kko\, ARICA 2\, Kosen 2R\, Magnaro II\, FSI-SAT 2 and Waseda-SAT 0-II. The
  mission was switched from Epsilon S to Electron in 2025. Rocket Lab's mis
 sion will be named "Kakushin Rising".\n-\nMAGNARO II are two small satelli
 tes developed by the Nagoya University to demonstrate formation flying tec
 hniques. The purpose is to develop a method to achieve resource saving\, h
 igh accuracy\, and formation formation by rotating and separating connecte
 d micro-satellites to form a formation\, and achieve simultaneous multi-po
 int observation and continuous Earth observation with micro-satellites. MA
 GNARO is launched as a 3U CubeSat sized package of 4.4kg that splits into 
 two satellites after deployment. One is 2U and the other is 1U in size. Th
 ey are connected by magnetism until their separation. After separating\, t
 hey will maintain formation flying between 2km to 500km distance from each
  other. Amateur radio operators will be able to use these satellites as re
 peaters for long-range communication.\n-\nKOSEN 2R is a 2U CubeSat satelli
 te developed by a partnership between the National Institute of Technology
  (KOSEN)\, Yonago College\, Gunma College\, and other educational bodies. 
 This 2.7kg satellites features a deployable Yagi-style directional antenna
  which extends after deployment. It is designed to study deformation of th
 e Earth’s crust under the sea floor. It makes use of dual reaction wheel
 s to maintain attitude control. It takes observations using a combination 
 of fish-eye camera lenses and magnetic sensors.\n-\nFSI-SAT 2 is a 1U Cube
 sat developed by the Future Science Institute as a low cost satellite feat
 uring a multi-spectral camera and on-board data processing system. It is d
 esigned to demonstrate that this technology can be deployed and operated a
 t this small scale and at low cost. The satellite has a mass of only 1.4kg
 .\n-\nWaseda-SAT 0-II is a 1U Cubesat developed by Waseda University as a 
 technology demonstrator for 3D-printed satellites. Its aim is to have zero
  fixing screws\, zero mechanical parts to be assembled together\, and zero
  debris. This is achieved by 3D-printing the entire chassis as a single el
 ement. It will be used to conduct experiments regarding deployment of memb
 rane surfaces which might be used as solar panels for power generation or 
 solar sail for propulsion. The total mass of the satellite is 1.2kg.
LOCATION:Onenui Station\, Māhia 4198\, Neuseeland
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