Hodoyoshi-3 is a Japanese micro-satellite launched in 2014. The satellite is built in 0.5x0.5x0.65m box-shape bus, optimized for piggy-back launch. All instruments are powered by solar cells mounted on the spacecraft body and two stub wings, with estimated electrical power of 50W.[1] For orbit-keeping, a hydrogen peroxide thruster is used. The latest information is available on FACEBOOK page.[2] The satellite was developed under the Funding Program for World-Leading Innovation R&D on Science and Technology.[3]
Mission type | Earth observation |
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Operator | NESTRA |
COSPAR ID | 2014-033F ![]() |
SATCAT no. | 40015 |
Website | At u-Tokyo.ac.jp |
Mission duration | 2942 days (ongoing) |
Spacecraft properties | |
Manufacturer | University of Tokyo |
Launch mass | 60 kg (130 lb) |
Start of mission | |
Launch date | 19:11, June 19, 2014 (UTC) (2014-06-19T19:11Z) |
Rocket | Dnepr |
Launch site | Dombarovsky |
Orbital parameters | |
Reference system | Geocentric |
Eccentricity | 0 |
Perigee altitude | 600 km (370 mi) |
Apogee altitude | 600 km (370 mi) |
Inclination | 97.9° |
Hodoyoshi-3 was launched from Dombarovsky (air base) site 13, Russia, on 19 June 2014 by a Dnepr rocket. Two-side communication with Earth was successfully achieved at 2nd pass over ground station.
The satellite is intended primarily for technology verification in space, main test piece being 2 Earth observation cameras with nominal 40 m GSD (Middle resolution camera: MCAM) and 200 m GSD (Low resolution camera: LCAM). MCAM is performing the spectroscopic observation of near-infrared rays, red, and three green bands by adopting a multi-band pass filter as a spectrum filter. Normalized Difference Vegetation Index(NDVI) drawn using near-infrared rays and a red band, It is well used to evaluation of the degrees of growth, such as agricultural products and trees, and soundness, and broad-based mapping of a vegetation index is attained by using the spectrum picture which MCAM acquires. Secondary mission is measurements of water level in rivers to monitor floods by using Store&Forward System.[4] Third mission is Hosted Payload. Hosted Payload mission consisted of 10 cm-cubic boxes on which users could install their own apparatuses for their own applications. Project members asked users in private partnership such as Sanrio corporation in order to explore new market of satellite utilization.
The satellite also included private/public partnership in the form of Hello Kitty, a popular character of the Sanrio corporation, on the satellite Hosted Payload box. Hello Kitty looks out a window of the craft to a view of Earth. Electronic message display was installed which operators could change characters on the display by sending commands from the ground station. Users can take photos of their messages with Hello Kitty figure and the view of the earth from the window. The inclusion is an attempt to get more private Japanese companies working with satellites and it is hoped will boost enthusiasm for space among Hello Kitty's many fans.[5]
Japanese space program | |||||||||||||
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Astronomical observation |
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Communications, broadcasting and navigation |
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Earth observation |
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Engineering tests |
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Human spaceflight |
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Lunar and planetary exploration |
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Private miniaturized satellites |
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Reconnaissance |
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← 2013 · Orbital launches in 2014 · 2015 → | |
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January | |
February | Progress M-22M – ABS-2 · Athena-Fidus – Türksat 4A – USA-248 – GPM Core · Ginrei · KSAT-2 · INVADER · OPUSAT · STARS-II · TeikyoSat-3 · ITF-1 |
March | |
April | USA-249 – Sentinel-1A – IRNSS-1B – Progress M-23M – Ofek-10 – USA-250 – EgyptSat 2 – SpaceX CRS-3 · KickSat · PhoneSat 2.5 · ALL-STAR/THEIA · SporeSat · TestSat-Lite – Luch 5V · KazSat-3 – KazEOSat 1 |
May | Kosmos 2495 – Ekspress AM4R – USA-251 – USA-252 – Kosmos 2496 · Kosmos 2497 · Kosmos 2498 · Kosmos 2499 – ALOS-2 · Raijin-2 · UNIFORM-1 · SOCRATES · SPROUT – Eutelsat 3B – Soyuz TMA-13M |
June | Kosmos 2500 – Deimos-2 · KazEOSat 2 · Hodoyoshi 3 · Hodoyoshi 4 · AprizeSat 9, 10 · BRITE-Montreal · BRITE-Toronto · BugSat 1 · SaudiSat-4 · TabletSat-Aurora · UniSat-6 (AeroCube-6 · ANTELSAT · Lemur-1 · Tigrisat) · DTUSat-2 · Duchifat-1 · NanoSatC-Br 1 · PACE · Perseus-M × 2 · PolyITAN-1 · POPSAT-HIP-1 · QB50P1 · QB50P2 · Flock-1c × 11 – SPOT 7 · CanX-4 · CanX-5 · AISat · VELOX-I |
July | OCO-2 – Gonets-M No. 8, 9, 10 – Meteor-M 2 · AISSat-2 · DX-1 · Relek · SkySat-2 · TechDemoSat-1 · UKube-1 – O3b × 4 (FM3, FM6, FM7, FM8) – CRS Orb-2 (Flock-1b × 28 · TechEdSat-4) – Orbcomm-2 × 6 – Foton-M No.4 – Progress M-24M – USA-253 · USA-254 · USA-255 – Georges Lemaître ATV |
August | USA-256 – AsiaSat 8 – Yaogan 20 A, B, C – WorldView-3 – Gaofen 2 · Heweliusz – Galileo FOC-1 · Galileo FOC-2 |
September | Chuangxin 1-04 · Lingqiao – AsiaSat 6 – Yaogan 21 · Tiantuo 2 – MEASAT 3b · Optus 10 – USA-257 – SpaceX CRS-4 – Soyuz TMA-14M – Olimp-K – Shijian XI-07 |
October | Himawari 8 – IRNSS-1C – Intelsat 30 · ARSAT-1 – Yaogan 22 – Ekspress AM6 – Chang'e 5-T1 · 4M – Shijian 11-08 – Cygnus CRS Orb-3 (Arkyd-3 · Flock-1d × 26 · GOMX-2 · RACE) – Progress M-25M – USA-258 – Meridian 7 |
November | Sasuke · Hodoyoshi 1 · Kinshachi 1 · Tsukushi · TSUBAME – Yaogan 23 – Yaogan 24 – Kuaizhou 2 – Soyuz TMA-15M – Kosmos 2501 |
December | Hayabusa2 · PROCYON · Shinen 2 · DESPATCH – Orion EFT-1 – DirecTV-14 · GSAT-16 – CBERS-4 – Yaogan 25 A, B, C – USA-259 – Yamal-401 – O3b × 4 (FM9 to FM12) – Kondor-E No.2 – IPM – Kosmos 2502 – Resurs-P No.2 – Yaogan 26 – Astra 2G – Fengyun 2-08 |
Launches are separated by dashes ( – ), payloads by dots ( · ). Crewed flights are underlined. Launch failures are in italics. Payloads deployed from other spacecraft are (enclosed in brackets). |