Launch 2021

Launch 2022

Launch 2023

Launch 2024

<img src="https://strapi.spacepi.space/uploads/MGU_Standart_Vizard_ion_d59729fcf6.png" alt="МГУ-Стандарт Vizard-ion.png" srcset="https://strapi.spacepi.space/uploads/thumbnail_MGU_Standart_Vizard_ion_d59729fcf6.png 232w,https://strapi.spacepi.space/uploads/small_MGU_Standart_Vizard_ion_d59729fcf6.png 500w,https://strapi.spacepi.space/uploads/medium_MGU_Standart_Vizard_ion_d59729fcf6.png 750w,https://strapi.spacepi.space/uploads/large_MGU_Standart_Vizard_ion_d59729fcf6.png 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="width:200px;">SC name</th><td>Vizard-ion</td></tr><tr><th style="width:200px;">NORAD ID</th><td>not assigned</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>not assigned</td></tr><tr><th>Call sign</th><td>RS68S</td></tr><tr><th>Frequencies</th><td>Transmitters: 436.87 MHz, 10.475 GHzReceiver: 436.87 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,098 kg</td></tr><tr><th>Payload</th><td>GNSS receiver, VERA plasma propulsion system, camera</td></tr><tr><th>Mission</th><td>Flight tests of the receiver of signals of global navigation satellite systems GLONASS/GPS, plasma propulsion system and optical camera of visible range.</td></tr><tr><th>Platform</th><td>Geoscan LLC</td></tr><tr><th>Launch date</th><td>is planned for 2024</td></tr><tr><th>Launch vehicle</th><td>&nbsp;</td></tr><tr><th>Status</th><td>Waiting for launch</td></tr></tbody></table></figure>The smallsat «Vizard-ion» of the MSU-STANDARD company was created on the basis of the Geoscan 3U satellite platform.«Vizard-ion» is designed for flight tests of the VERA (plasma propulsion system) and studying the ionosphere by the receiver of signals (GLONASS/GPS). Additional payload of the cubesat is a camera with a resolution of 1632x1232 (2MP).

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Smallsat of the «MSU-STANDARD» company for the ionosphere studies

Vizard-ion

<img src="https://strapi.spacepi.space/uploads/Gorizont_transportnoe_polozhenie_e0a218d142.png" alt="Горизонт (транспортное положение).png" srcset="https://strapi.spacepi.space/uploads/thumbnail_Gorizont_transportnoe_polozhenie_e0a218d142.png 232w,https://strapi.spacepi.space/uploads/small_Gorizont_transportnoe_polozhenie_e0a218d142.png 500w,https://strapi.spacepi.space/uploads/medium_Gorizont_transportnoe_polozhenie_e0a218d142.png 750w,https://strapi.spacepi.space/uploads/large_Gorizont_transportnoe_polozhenie_e0a218d142.png 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="width:200px;">SC name</th><td>Horizon</td></tr><tr><th>NORAD ID</th><td>not assigned</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>not assigned</td></tr><tr><th>Call sign</th><td>RS59S</td></tr><tr><th>Frequencies</th><td>Transmission: 435 MHz, 436 MHz,10 GHz,2.4GHz.Reception: 435 MHz, 436 MHz, 2.4GHz, 863-869 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,2 kg</td></tr><tr><th>Payload</th><td>- Electronic Components Research Module;- solar panel deployment system;- orientation system based on flywheel engines;- 3-band transceivers;&nbsp;- camera.</td></tr><tr><th>Mission</th><td>Study the effect of radiation on electronic components, tests of an active orientation system based on flywheel engines, photo shooting the Earth's surface, exploring the possibilities of radio lines using linear frequency manipulation and image transmission using fountain codes, studying the degradation of the characteristics of solar panels of various compositions under the influence of space factors</td></tr><tr><th>Platform</th><td>Geoscan LLC</td></tr><tr><th>Launch date</th><td>is planned for 2024</td></tr><tr><th>Launch vehicle</th><td>&nbsp;</td></tr><tr><th>Status</th><td>Waiting for launch</td></tr></tbody></table></figure>The «Horizon» smallsat was developed by the team of&nbsp;<a href="https://www.voenmeh.ru/" target="_blank" rel="noopener noreferrer">Baltic State Technical University&nbsp;«Voenmeh» D. F. Ustinov</a>&nbsp;on the basis of the Geoscan 3U satellite platform.The payload includes:1) Solar panel module designed to study the degradation of the characteristics of different solar panels under the influence of space factors;2) Electronic components research module. It includes advanced magnetoresistive random access memory (MRAM) chips, which are tested for stability in conditions of space radiation;3) The CubeSat mechanical orientation unit, implemented on the basis of electric motors. When controlling the flywheel system, the satellite is oriented along three axes;4) Payload management system. It consists of transceiver modules operating in the VHF and S bands, and a computing unit with a camera resolution of 3840x2160 pixels.<figure class="image"><img src="https://strapi.spacepi.space/uploads/large_6_B4_A6582_36bb481301_69d508d548.jpg" alt="large_6_B4_A6582_36bb481301.jpg" srcset="https://strapi.spacepi.space/uploads/thumbnail_large_6_B4_A6582_36bb481301_69d508d548.jpg 234w,https://strapi.spacepi.space/uploads/small_large_6_B4_A6582_36bb481301_69d508d548.jpg 500w,https://strapi.spacepi.space/uploads/medium_large_6_B4_A6582_36bb481301_69d508d548.jpg 750w," sizes="100vw"><figcaption>In the photo: on the end of the CubeSat, an 868 MHz patch antenna is on top, and a 2.4 GHz patch antenna is on the bottom</figcaption></figure><figure class="image"><img src="https://strapi.spacepi.space/uploads/large_6_B4_A6585_3d37e3f55f_910838bc75.jpg" alt="large_6_B4_A6585_3d37e3f55f.jpg" srcset="https://strapi.spacepi.space/uploads/thumbnail_large_6_B4_A6585_3d37e3f55f_910838bc75.jpg 234w,https://strapi.spacepi.space/uploads/small_large_6_B4_A6585_3d37e3f55f_910838bc75.jpg 500w,https://strapi.spacepi.space/uploads/medium_large_6_B4_A6585_3d37e3f55f_910838bc75.jpg 750w," sizes="100vw"><figcaption>On the right in the picture is an open solar panels module</figcaption></figure>

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The second cubesat of BSTU «VOENMEH» with experimental developments of students

Horizon

<img src="https://strapi.spacepi.space/uploads/RTU_MIREA_1_transportnoe_polozhenie_41b7f26ab9.png" alt="РТУ МИРЭА1 (транспортное положение).png" srcset="https://strapi.spacepi.space/uploads/thumbnail_RTU_MIREA_1_transportnoe_polozhenie_41b7f26ab9.png 245w,https://strapi.spacepi.space/uploads/small_RTU_MIREA_1_transportnoe_polozhenie_41b7f26ab9.png 500w,https://strapi.spacepi.space/uploads/medium_RTU_MIREA_1_transportnoe_polozhenie_41b7f26ab9.png 750w,https://strapi.spacepi.space/uploads/large_RTU_MIREA_1_transportnoe_polozhenie_41b7f26ab9.png 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="width:200px;">SC name</th><td>RTU MIREA1</td></tr><tr><th>NORAD ID</th><td>not assigned</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>not assigned</td></tr><tr><th>Call sign</th><td>RS51S</td></tr><tr><th>Frequencies</th><td>436 MHz transceiver (center frequency 436.320 MHz)10 GHz transmitter (center frequency 10475.0 MHz)</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,064 kg</td></tr><tr><th>Payload</th><td>1. Optical-electronic equipment of the visible range.2. On-board navigation receiver GLONASS/GPS signals.3. Transceiver module for organizing an inter-satellite communication channel with a small spacecraft «TUSUR-GO».</td></tr><tr><th>Mission</th><td>Experiments on inter-satellite communication, flight tests of an optical camera and a receiver of signals (GLONASS/GPS).</td></tr><tr><th>Platform</th><td>Geoscan LLC</td></tr><tr><th>Launch date</th><td>is planned for 2024</td></tr><tr><th>Launch vehicle</th><td>&nbsp;</td></tr><tr><th>Status</th><td>Waiting for launch</td></tr></tbody></table></figure>The smallsat of <a href="https://english.mirea.ru/" target="_blank" rel="noopener noreferrer">the Russian Technological University MIREA</a> was created on the basis of the Geoscan 3U satellite platform.The RTU MIREA1 spacecraft is designed for flight tests of an optical camera of the visible range and a receiver of signals from global navigation satellite systems GLONASS/GPS, conducting an experiment on inter-satellite communication using a receiving and transmitting module, as well as for conducting educational activities within the framework of the Space-π project.The use of an optical camera of the visible range will allow us to study aspects of the formation of the Earth's cloud cover.&nbsp;The use of the receiver of signals of global navigation satellite systems GLONASS / GPS allows the use of the method of radio-exchange sensing of the ionosphere. For this method, the sources of radio signals are the GLONASS/GPS spacecraft, and the receiver should be installed on a low-orbit spacecraft. Due to the influence of the ionosphere, the low-orbit spacecraft can receive navigation signals while being out of the line of sight of the navigation spacecraft.A transceiver module is installed on the RTU MIREA1 spacecraft to provide an inter-satellite communication channel with the&nbsp; <a href="https://en.spacepi.space/satellites/tusur-go/" target="_blank" rel="noopener noreferrer">«TUSUR-GO»</a> spacecraft.

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RTU MIREA satellite for ionospheric research

RTU MIREA1 

<img src="https://strapi.spacepi.space/uploads/TUSUR_GO_2_b22741df09.png" alt="ТУСУР GO (2).png" srcset="https://strapi.spacepi.space/uploads/thumbnail_TUSUR_GO_2_b22741df09.png 231w,https://strapi.spacepi.space/uploads/small_TUSUR_GO_2_b22741df09.png 500w,https://strapi.spacepi.space/uploads/medium_TUSUR_GO_2_b22741df09.png 750w,https://strapi.spacepi.space/uploads/large_TUSUR_GO_2_b22741df09.png 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="width:200px;">SC name</th><td>TUSUR GO</td></tr><tr><th>NORAD ID</th><td>not assigned</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>not assigned</td></tr><tr><th>Call sign</th><td>RS78S</td></tr><tr><th>Frequencies</th><td>Transmitters: 437,73 MHz, 10,475 GHzReceiver: 437,73 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>2,443 kg</td></tr><tr><th>Payload</th><td>Transceiver module, GNSS receiver and camera</td></tr><tr><th>Mission</th><td>Flight tests of a satellite communication device for transmitting data from monitoring objects to a ground terminal, including the possibility of retransmission via another spacecraft.</td></tr><tr><th>Platform</th><td>Geoscan LLC</td></tr><tr><th>Launch date</th><td>is planned for 2024</td></tr><tr><th>Launch vehicle</th><td>&nbsp;</td></tr><tr><th>Status</th><td>Waiting for launch</td></tr></tbody></table></figure>The satellite of <a href="https://tusur.ru/en" target="_blank" rel="noopener noreferrer">Tomsk State University</a> of Control Systems and Radioelectronics was created on the basis of the Geoscan 3U satellite platform.TUSUR GO is designed for flight tests of a satellite communication device for transmitting data from monitoring objects to a ground terminal, including the possibility of retransmission through another spacecraft, as well as conducting educational activities within the framework of the Space-π project.The payload of the device includes:1) A transceiver module to provide an inter-satellite communication channel with the spacecraft <a href="https://en.spacepi.space/satellites/rtu-mirea-1/" target="_blank" rel="noopener noreferrer">«RTU MIREA1»</a>;2) GNSS receiver in the frequency range L1 (GPS, GLONASS), E1 Galileo;3) Camera module: angle of view (FOV): 66 degrees, resolution 2 MP.<figure class="image image_resized" style="width:50%;"><img src="https://strapi.spacepi.space/uploads/Emblema_Missii_TUSUR_GO_8c15b1714f.jpg" alt="Эмблема_Миссии_TUSUR_GO.jpg" srcset="https://strapi.spacepi.space/uploads/thumbnail_Emblema_Missii_TUSUR_GO_8c15b1714f.jpg 156w,https://strapi.spacepi.space/uploads/small_Emblema_Missii_TUSUR_GO_8c15b1714f.jpg 500w,https://strapi.spacepi.space/uploads/medium_Emblema_Missii_TUSUR_GO_8c15b1714f.jpg 750w,https://strapi.spacepi.space/uploads/large_Emblema_Missii_TUSUR_GO_8c15b1714f.jpg 1000w," sizes="100vw"><figcaption>Mission emblem</figcaption></figure>

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Spacecraft of Tomsk State University of Control Systems and Radioelectronics for inter-satellite communication

TUSUR GO

<img src="/uploads/52794735676_c5827012e0_k_785593a49a.jpg" alt="52794735676_c5827012e0_k.jpg" srcset="/uploads/thumbnail_52794735676_c5827012e0_k_785593a49a.jpg 234w,/uploads/small_52794735676_c5827012e0_k_785593a49a.jpg 500w,/uploads/medium_52794735676_c5827012e0_k_785593a49a.jpg 750w,/uploads/large_52794735676_c5827012e0_k_785593a49a.jpg 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="vertical-align:top;">SC name</th><td><a href="https://sputnix.ru/en/satellites-sputnix/planned-missions/svyatobor-1" target="_blank" rel="noopener noreferrer">Svyatobor-1</a></td></tr><tr><th style="vertical-align:top;">NORAD ID</th><td><a href="https://www.n2yo.com/satellite/?s=57187" target="_blank" rel="noopener noreferrer">57187</a></td></tr><tr><th style="vertical-align:top;"><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3671-2023-009</td></tr><tr><th style="vertical-align:top;">Call sign</th><td>RS60S</td></tr><tr><th style="vertical-align:top;">Frequencies</th><td>437,875 MHz</td></tr><tr><th style="vertical-align:top;">Format</th><td>3U</td></tr><tr><th style="vertical-align:top;">Weight</th><td>3,4 kg</td></tr><tr><th style="vertical-align:top;">Payload</th><td>- thermal imaging camera with an angular shooting resolution of 480 mkrad/pixels,- visible range color camera with a resolution of 31 mkrad/pixels,- experimental plasma propulsion system VERA&nbsp;</td></tr><tr><th style="vertical-align:top;">Mission</th><td>Control of forest fires and other natural disasters</td></tr><tr><th style="vertical-align:top;">Platform</th><td>SPUTNIX LLC</td></tr><tr><th style="vertical-align:top;">Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th style="vertical-align:top;">Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Active</td></tr></tbody></table></figure>Kubsat of the&nbsp;National Research Nuclear University&nbsp;«MEPhI».&nbsp;The satellite will track forest fires, equipped with a thermal imaging camera, which will quickly detect fires and thermal anomalies on the Earth's surface. A visible-range color camera is needed for photofixation of fires with a resolution of 15-17 meters per pixel. To correct and maintain the orbit on the satellite, there is a propulsion system developed by the <a href="https://laplas.mephi.ru/" target="_blank" rel="noopener noreferrer">LaPlace</a> Institute and students of the MEPhI National Research University.&nbsp;<figure class="image"><img src="/uploads/doc184159847_657363550_ac40d0bceb.jpg" alt="doc184159847_657363550.jpg" srcset="/uploads/thumbnail_doc184159847_657363550_ac40d0bceb.jpg 208w,/uploads/small_doc184159847_657363550_ac40d0bceb.jpg 500w,/uploads/medium_doc184159847_657363550_ac40d0bceb.jpg 750w,/uploads/large_doc184159847_657363550_ac40d0bceb.jpg 1000w," sizes="100vw"><figcaption>Payload module</figcaption></figure><figure class="image"><img src="/uploads/doc184159847_657363561_f0bbd5c7ac.jpg" alt="doc184159847_657363561.jpg" srcset="/uploads/thumbnail_doc184159847_657363561_f0bbd5c7ac.jpg 205w,/uploads/small_doc184159847_657363561_f0bbd5c7ac.jpg 500w,/uploads/medium_doc184159847_657363561_f0bbd5c7ac.jpg 750w,/uploads/large_doc184159847_657363561_f0bbd5c7ac.jpg 1000w," sizes="100vw"><figcaption>Tests of the VERA propulsion system</figcaption></figure>

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Cubesat with modified plasma engine «VERА» and thermal imaging camera

Svyatobor-1

<img src="/uploads/Ahmat_1_7564081887.jpeg" alt="Ахмат-1.jpeg" srcset="/uploads/thumbnail_Ahmat_1_7564081887.jpeg 245w,/uploads/small_Ahmat_1_7564081887.jpeg 500w,/uploads/medium_Ahmat_1_7564081887.jpeg 750w,/uploads/large_Ahmat_1_7564081887.jpeg 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th>SC name</th><td>Akhmat-1</td></tr><tr><th>NORAD ID</th><td>57208</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3645-2023-009</td></tr><tr><th>Call sign</th><td>RS41S</td></tr><tr><th>Frequencies</th><td>437,05 MHz, 1090 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>2,5 kg</td></tr><tr><th>Payload</th><td>ADS-B module</td></tr><tr><th>Mission</th><td>Aircraft monitoring</td></tr><tr><th>Platform</th><td>Southwest State University&nbsp;</td></tr><tr><th>Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th>Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Non-Operational</td></tr></tbody></table></figure>Akhmat-1 – satellite of the&nbsp;Kadyrov&nbsp;Chechen&nbsp;State&nbsp;University.ADS-B module allows pilots of aircraft, as well as air traffic controllers at the ground reporting points to monitor the movement of the aircraft with great accuracy and receive data on its location in real time. Thus, communication with the aircraft is possible along the entire route of its movement.The transfer of aircraft location data is possible and widely practiced via large communication satellites, but by a small number of air traffic controllers due to the high cost of transmitting information.&nbsp;The technology of data transmission from the aircraft to the reporting points is tested for the first time on the SC «Akhmat-1».&nbsp;One ADS-B module installed on one small spacecraft will provide a signal reception area for at least 1500 km.&nbsp;&nbsp;<figure class="image image_resized" style="width:50%;"><img src="/uploads/azn_v_e4d5665188.jpg" alt="азн в.jpg" srcset="/uploads/thumbnail_azn_v_e4d5665188.jpg 153w,/uploads/small_azn_v_e4d5665188.jpg 489w," sizes="100vw"><figcaption>ADS-B module</figcaption></figure><figure class="image image_resized" style="width:75%;"><img src="/uploads/photo1681302452_1_62b557d524.jpeg" alt="photo1681302452-1-.jpeg" srcset="/uploads/thumbnail_photo1681302452_1_62b557d524.jpeg 88w,/uploads/small_photo1681302452_1_62b557d524.jpeg 281w,/uploads/medium_photo1681302452_1_62b557d524.jpeg 422w,/uploads/large_photo1681302452_1_62b557d524.jpeg 563w," sizes="100vw"></figure>

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The first satellite of the Chechen Republic. Equipped with the ADS-B module for monitoring aircraft

Akhmat-1 

<img src="/uploads/Vizard_meteo_bda37bb6c8.jpg" alt="Vizard-meteo.jpg" srcset="/uploads/thumbnail_Vizard_meteo_bda37bb6c8.jpg 234w,/uploads/small_Vizard_meteo_bda37bb6c8.jpg 500w,/uploads/medium_Vizard_meteo_bda37bb6c8.jpg 750w,/uploads/large_Vizard_meteo_bda37bb6c8.jpg 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th style="vertical-align:top;width:200px;">SC name</th><td><a href="https://sputnix.ru/en/satellites-sputnix/planned-missions/vizard-meteo" target="_blank" rel="noopener noreferrer">Vizard-meteo</a></td></tr><tr><th style="vertical-align:top;">NORAD ID</th><td><a href="https://www.n2yo.com/satellite/?s=57189#results" target="_blank" rel="noopener noreferrer">57189</a></td></tr><tr><th style="vertical-align:top;"><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3662-2023-009</td></tr><tr><th style="vertical-align:top;">Call sign</th><td>RS38S</td></tr><tr><th style="vertical-align:top;">Frequencies</th><td>437.83 MHz</td></tr><tr><th style="vertical-align:top;">Format</th><td>3U</td></tr><tr><th style="vertical-align:top;">Weight</th><td>2,98 kg</td></tr><tr><th style="vertical-align:top;">Payload</th><td>A medium-resolution RGB remote sensing camera with a pixel projection of 50 m/pixel, a low-resolution RGB remote sensing camera with a pixel projection of 250 m/pixel.</td></tr><tr><th style="vertical-align:top;">Mission</th><td>Monitoring the formation of dangerous meteorological phenomena in the atmosphere and forecasting the development of the meteorological situation</td></tr><tr><th style="vertical-align:top;">Platform</th><td>SPUTNIX LLC</td></tr><tr><th style="vertical-align:top;">Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th style="vertical-align:top;">Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Active</td></tr></tbody></table></figure>Vizard-meteo CubeSat belongs to the Moscow company «NIS» LLC.&nbsp;Vizard-meteo has 2 Earth remote sensing cameras on board. They will help to obtain images for monitoring oil and petroleum product spills in the Arctic zone, as well as predict the development of the situation on the Northern Sea Route, identify the formation of dangerous meteorological phenomena.As part of educational purpose of the spacecraft, scholars and students will receive space data from Vizard-meteo and analyze them for environmental and weather phenomena in the waters of the Northern Polar Region.<img src="/uploads/NIS_1_obr_978cceca33.jpg" alt="НИС 1 (обр.).jpg" srcset="/uploads/thumbnail_NIS_1_obr_978cceca33.jpg 210w,/uploads/small_NIS_1_obr_978cceca33.jpg 500w,/uploads/medium_NIS_1_obr_978cceca33.jpg 750w,/uploads/large_NIS_1_obr_978cceca33.jpg 1000w," sizes="100vw">

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Meteorological satellite of the Moscow company «NIS»

Vizard-meteo

<img src="/uploads/Kuz_GTU_1_31ec0dae08.jpg" alt="КузГТУ(1).jpg" srcset="/uploads/thumbnail_Kuz_GTU_1_31ec0dae08.jpg 234w,/uploads/small_Kuz_GTU_1_31ec0dae08.jpg 500w,/uploads/medium_Kuz_GTU_1_31ec0dae08.jpg 750w,/uploads/large_Kuz_GTU_1_31ec0dae08.jpg 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th>SC name</th><td><a href="https://sputnix.ru/en/satellites-sputnix/planned-missions/kuzgtu-1" target="_blank" rel="noopener noreferrer">KuzSTU-1</a></td></tr><tr><th>NORAD ID</th><td><a href="https://www.n2yo.com/satellite/?s=57217" target="_blank" rel="noopener noreferrer">57217</a></td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3646-2023-009</td></tr><tr><th>Call sign</th><td>RS47S</td></tr><tr><th>Frequencies</th><td>437.100 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,4 kg</td></tr><tr><th>Payload</th><td>Control board, 3 vibration sensors (Globaltest AP2037-500) and an electromechanical emulator of a part with internal voltages</td></tr><tr><th>Mission</th><td>Formation of physical and mathematical scientific groups and approaches in the design of small spacecraft</td></tr><tr><th>Platform</th><td>SPUTNIX LLC</td></tr><tr><th>Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th>Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Non-Operational</td></tr></tbody></table></figure>KuzSTU-1 is the second satellite of <a href="https://en.kuzstu.ru/" target="_blank" rel="noopener noreferrer">the Kuzbass State Technical University</a> launched within the framework of the Space-π project.The payload of the spacecraft consists of a control board, three vibration sensors (Globaltest AP2037-500) located in mutually perpendicular orientations on the frame of the MC, and an electromechanical emulator of a part with internal voltages.The control board provides bidirectional data transfer between the Sputnix CubeSat (SXC) OrbiCraft-Pro platform and the KuzSTU-1 payload.&nbsp;The electromechanical emulator represents a support and a movable element in the form of an elastic beam, one end of which has a hinge attachment, and the other end is movable. The moving element is moved by a stepper motor with a gearbox. A load cell is also attached to the movable element to monitor the level of internal stresses.&nbsp;<img src="/uploads/kuzgtu_pn_d55c4592f3.jpg" alt="кузгту пн.jpg" srcset="/uploads/thumbnail_kuzgtu_pn_d55c4592f3.jpg 235w,/uploads/small_kuzgtu_pn_d55c4592f3.jpg 500w,/uploads/medium_kuzgtu_pn_d55c4592f3.jpg 750w," sizes="100vw">

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Spacecraft to study the vibro-thermal response of the SC frame in space flight conditions

KuzSTU-1

<img src="/uploads/1_3_1_01d3c4dd6d.jpg" alt="1(3)(1).jpg" srcset="/uploads/thumbnail_1_3_1_01d3c4dd6d.jpg 156w,/uploads/small_1_3_1_01d3c4dd6d.jpg 500w,/uploads/medium_1_3_1_01d3c4dd6d.jpg 750w," sizes="100vw"><figure class="table"><table><tbody><tr><th>SC name</th><td>ReshUCube-2</td></tr><tr><th>NORAD ID</th><td>not specified (presumably 57168)</td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3670-2023-009</td></tr><tr><th>Call sign</th><td>RS37S</td></tr><tr><th>Frequencies</th><td>1 channel: 435.640 MHz2 channel: 435.742 MHzamateur radio repeater: 436.675 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,45 kg</td></tr><tr><th>Payload</th><td>A connected module for experiments with Earth-Space, Space-Space, Internet of Things communication protocols; a technological observation camera; a module for flight experiments with a domestic component base.</td></tr><tr><th>Mission</th><td>Flight experiments with promising network protocols for building satellite networks, Internet of Things networks, low-speed integrated Internet networks.</td></tr><tr><th>Platform</th><td>LLC&nbsp;«NILAKT DOSAAF»</td></tr><tr><th>Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th>Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Active</td></tr></tbody></table></figure>ReshUCube-2 is the second satellite of the Reshetnev Siberian State University of Science and Technology.The ReshUCube-2 space mission continues the concept of a «Сonfigurable Space Laboratory» laid down in the <a href="https://en.spacepi.space/satellites/resh-u-cube-1/" target="_blank" rel="noopener noreferrer">ReshUCube-1 </a>mission.However, the goals of experiments has changed. Within the framework of ReshUCube-2, it is planned to conduct experiments with promising communication protocols that will allow building an integrated data transmission network combining the inter-satellite communication segment with the ground segment of the terminals of the Internet of Things network. &nbsp;The results of the ReshUCube-2 space mission will be used in the ReshUCube-3 mission, within which 4 nanosatellites will be launched and an experimental integrated network will be created on this basis.&nbsp;Scholars of the Krasnoyarsk and Yakutia will take part in conducting space experiments to study network protocols and communication characteristics of an integrated network, try to create their own Internet of Things device and receive a signal from this device via a nanosatellite to a ground terminal.&nbsp;

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The second SibGU satellite with several experiments on board

ReshUCube-2

<img src="/uploads/OGU_Nanozond_1_acaf98dcd6.jpg" alt="ТюмГУ-2" srcset="/uploads/thumbnail_OGU_Nanozond_1_acaf98dcd6.jpg 234w,/uploads/small_OGU_Nanozond_1_acaf98dcd6.jpg 500w,/uploads/medium_OGU_Nanozond_1_acaf98dcd6.jpg 750w,/uploads/large_OGU_Nanozond_1_acaf98dcd6.jpg 1000w," sizes="100vw"><figure class="table"><table><tbody><tr><th>SC name</th><td><a href="https://sputnix.ru/en/satellites-sputnix/planned-missions/utmn-2" target="_blank" rel="noopener noreferrer">UTMN-2</a></td></tr><tr><th>NORAD ID</th><td><a href="https://www.n2yo.com/satellite/?s=57203" target="_blank" rel="noopener noreferrer">57203</a></td></tr><tr><th><a href="https://www.unoosa.org/oosa/osoindex/search-ng.jspx?lf_id=" target="_blank" rel="noopener noreferrer">Number in the Register</a></th><td>3663-2023-009</td></tr><tr><th>Call sign</th><td>RS27S</td></tr><tr><th>Frequencies</th><td>435-438 MHz, 485 MHz</td></tr><tr><th>Format</th><td>3U</td></tr><tr><th>Weight</th><td>3,97 kg</td></tr><tr><th>Payload</th><td>— detection node;— analog and digital electronics board (2 pcs.)— interface card (1 pc.)</td></tr><tr><th>Mission</th><td>Remote diagnostics of the troposphere and water reservoirs by satellite infrared thermometry. Prospect use of the SC in system «Smart City».</td></tr><tr><th>Platform</th><td>SPUTNIX LLC</td></tr><tr><th>Launch date</th><td>27.06.23, the Vostochny cosmodrome</td></tr><tr><th>Launch vehicle</th><td>LV «Soyuz-2.1b» with US «Fregat»</td></tr><tr><th>Status</th><td>Active</td></tr></tbody></table></figure>Satellite of the Tyumen State University is dedicated for environmental monitoring of the Tyumen region. The spacecraft was assembled as part of the project of remote diagnostics of the troposphere and water reservoirs by satellite infrared thermometry. The payload was developed at the Moscow State University Research Institute of Nuclear Physics.&nbsp;UTMN-2 will take pictures of clouds and lakes so scholars will be able to remotely determine their temperature and contribute to improving the reliability of weather forecasts.&nbsp;The satellite is also planned to be used as part of the «Smart City» system. Space data allows you to find a free parking lot, forecast traffic jams, see the scale of certain natural phenomena.&nbsp;

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ТюмГУ-2

Tyumen State University CubeSat for diagnostics of the troposphere and water reservoirs of the Earth

Project satellites

New items in the encyclopedia and the latest news.

New items in the encyclopedia
and the latest news.