OPUSAT-II

Foto OPUSAT-II

47924
Nummer im Katalog Spacetrack
1998-11-20
In die Umlaufbahn bringen
2022-05-01
8563 Tage
390.03 km
Höhe Durchschnitt
27642.45 km/h
Durchschnittsgeschwindigkeit

Informationen über den Satelliten. OPUSAT-II

Name im Katalog Spacetrack OPUSAT-II
In die Umlaufbahn bringen 1998-11-20
Datum 2022-05-01
Tage im Orbit 8563
Herkunftsland/-organisation Japonia (JPN)
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. TYMSC (Baikonur Cosmodrome, Kazakhstan)
WWW hier
Kategorie

Informationen über OPUSAT-II

WARP-01 is a 1U CubeSat developed by a Japanese space startup, Warpspace Inc., and University of Tsukuba and launched by a Japanese launch service provider, Space BD Inc.  
WARP-01?s mission objective is:
To demonstrate new satellite bus components: the University of Tsukuba and Warpspace Inc. developed new and cost-effective satellite bus components, a UHF communications module, electric power supply module, on board computer module with GPS receiver IC, and an aluminum chassis. The WARP-01 CubeSat demonstrates the performance of these new components in space.
To carry wedding memorial plates into space: as part of a commercial mission, WARP-01 carries wedding memorial plates made of titanium into space.
To gather images of the Earth and space: after deployment from the International Space Station (ISS), WARP-01 deploys a panel that has an attached camera and sensors to gather images of the Earth and space.
To survey the radiation environment in space: WARP-01 demonstrates the performance of a radiation sensor to survey the radiation environment in low-Earth orbit. Specifically, the sensor contains a micro SD card to observe single event upsets (SEUs) caused by beta radiation.
To survey the radio environment in space: WARP-01 demonstrates software defined radio (SDR), and surveys the radio environment in space. Specifically, the SDR receives signals in the 430MHz amateur radio band and analyzes the radio field intensity.
Using the COTS one-chip transceiver IC, demonstrate functionalities of original designed and developed transmitter in space environment by radio-wave transmission of CW beacon and various digital modulation such as GFSK, 4GFSK, FSK, 4FSK. This transceiver is designed from the scratch with ham-radio spirits. - To make satellite ham radio communication more popular, introduce fast, low-cost and flexible digital transceiver technology for worldwide amateur.

Durchschnittshöhe der Orbitalbahn. OPUSAT-II

Durchschnittsgeschwindigkeit OPUSAT-II

Durchschnitt OPUSAT-II

Aktualisierungsdatum.: 2022-05-05 09:05:17