ShindaiSat

Japanese small technology demonstration satellite. ShindaiSat was launched on February 27, 2014 aboard a H-IIA 202 from Tanegashima. Latest status in GCAT: reentered (orbital decay) (Nov 24, 2014).

COSPAR 2014-009ANORAD 39572Japan

Identity

Name in GCAT: Ginrei
Common name: ShindaiSat
Payload designation: ShindaiSat
International designator: 2014-009A
NORAD catalog number: 39572
GCAT identifier: S39572
UN registration: ST/SG/SER.E/735

Mission

Mission type: Technology
Use: Amateur / academic
Program: Shindai
Owner: Shinshu U
Country: Japan
Builder: Shinshu University
Platform (bus): Shindai

Launch

Date: February 27, 2014 · 18:37 UTC
Launch record: 2014-009Success
Rocket: H-IIA 202
Spaceport: Tanegashima · pad Y

Orbit and fate

Orbit class (GCAT): LLEO/I
Perigee: 387 km
Apogee: 405 km
Inclination: 65.02°
Status: Reentered (orbital decay)
Status date: November 24, 2014
Last known active: May 26, 2014
End of operations: Nov 24, 2014

Size

Mass: 33 kg
Dry mass: 33 kg
Length: 0.5 m
Diameter: 0.40 m
Span: 0.5 m

Launched together

ITF-1Technology · Tsukuba U Global Precipitation MeasurementEarth science · GSFC OPUSatTechnology · Osaka Pref. U.TeikyoSat-3Biology · Teikyo INVADEREducation · Tama Hayato-2Technology · Kagoshima U Space Tethered Autonomous Robotic Satellite IITechnology · Kagawa U

Source: GCAT payload, deep-space and lander catalogs, Jonathan C. McDowell (CC BY 4.0); Wikidata Q16060295 (CC0).