Спутник технологический. STSAT 2C. [Редактировать]

КА STSAT-2C выведен на целевую эллиптическую орбиту высотой около 300 км. Планируется, что этот спутник массой 100 кг будет находиться в космосе в течение одного года и проведет серию экспериментов и исследований различного назначения. Он разработан Корейским ведущим научно-техническим институтом KAIST (Korea Advanced Institute of Science and Technology) в г. Тэджон, пров. Чхунчхон-Намдо, который считается научно-технической столицей Южной Кореи.

Перечень экспериментов:

  • LRA (Laser Retro-reflector Array) – определение положение корабля посредством лазера;
  • SREM (Space Radiation Effects Monitor) – измерение радиации на орбите;
  • Langmuir probe – изучение свойств плазмы на низкой орбите;
  • FSO (Femto second Laser Oscillator) – лазерный излучатель;
  • RWA (Reaction Wheel Assembly) IRS – инфракрасный датчик.   

 

Дополнительные наименования

#НаименованияПоиск в новостяхПоиск в документах
139068НайтиНайти

Дополнительная классификация

#Наименования
1Страна оператор(владелец) - Южная Корея
2Тип оператора(владельца) - государственный
3Тип орбиты - НОО
4Страна производитель - Южная Корея

Технические характеристики

#ХарактеристикаЗначение
1Масса, кг100

Характеристики орбиты

#ХарактеристикаЗначение
1Наклонение, град80.3
2Апогей, км1324.3
3Апогей, км1322.7
4Перигей, км298.7
5Перигей, км298.6
6Период, минут101.0
7Период, минут100.9
8Длинный диаметр эллипса, км7182
9Длинный диаметр эллипса, км7181

Пусковые характеристики

#ХарактеристикаЗначение
1Код NSSDC2013-003A

Информация об удачном запуске

#ХарактеристикаЗначение
1Дата пуска2013-01-31 at 07:00:00 UTC
2Полезная нагрузка 1xSTSAT 2C
3Ракета-носитель 1xKSLV 1

Найдено 88 документов по запросу «STSAT 2C». [Перейти к поиску]


Дата загрузки: 2017-03-28
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0.03/5
... industry Naro rocket, KOMPSAT-5 and STSAT-3. policies and conduct studies and... not high, the government is STSAT-3. establishing and implementing plans to... STSAT-1 2006 KOMPSAT-2 2009/2010 STSAT-2 2010 COMS 2012 KOMPSAT-3 2013 STSAT-2C 2020... satellite 1 2014 KOMPSAT-3A 2013 STSAT-3 2013 KOMPSAT-5 21 Space Programs... PSLV on May 26, 1999. STSAT-1 STSAT-1 was developed for the purpose... a space program initiated by Korea. STSAT-1 was successfully launched on September... Russia. The STSAT-1 ended its operation in 2009. 22 STSAT-2 STSAT-2 is a 100kg... purposes, the low-orbit satellite STSAT-2 rotates around 300~1500km above... forecast and geological exploration purposes. STSAT-2 was to be launched into...’s atmosphere Observation plans to use STSAT-2 failed, and on January 30...-1) rocket, the STSAT-2C was launched instead of the STSAT-2. STSAT-3 STSAT-3(Science and Technology... the KAIST Satellite Research Center. STSAT-3 is Korea’s first infrared space... from Yasny base in Russia. STSAT-3 was launched on the Russian... hours after it was launched, STSAT-3 passed near South Korean skies... ground station at 10:10 p.m. STSAT-3 is mounted with MIRIS(Multi...) and COMIS(Compact Imaging System). STSAT-2C STSAT-2C is the scienced and technology... numbered STSAT-2C, it is different from the previous STSAT-2(STSAT-2A and STSAT-2B) launched on the first and second flights of KSLV-I . STSAT-2C... vehicle to launch a 100kg-class STSAT into the low-earth orbit... mounted with Naro STSAT-2C(Science and Technology Satellite-2C). Currently, development is...



Дата загрузки: 2017-06-15
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0.12/5
... the Science and Technology Satellite (STSAT)-2C as one of ILRS prediction... Consolidated Prediction Format (CPF). The STSAT-2C is the first Korean satellite... main provider of CPFs for STSAT-2C is the Korea Advanced Institute... center consistently provides CPFs for STSAT-2C. However, KAI CPFs based on... for orbit determination (OD) for STSAT-2C is SLR observations, and therefore... history of KAS CPFs for STSAT-2C generation is summarized. We will... for more SLR tracking for STSAT-2C.  Orbit Determination Using SLR  Orbit... Albedo pressure Empirical acceleration GGM-2C (200 by 200) JPL DE... sparse SLR tracking condition of STSAT-2CSTSAT-2C : 204 passes and 2,215 normal... prediction center (KAS): SLR-based STSAT-2C CPFs generation  KAS CPFs test...) Orbit determination and analysis for STSAT-2C, 18th International Workshop on Laser... The authors deeply appreciate the STSAT-2C mission operation and SLR support... stations for trying to track STSAT-2C using KAS CPFs. The authors...



Дата загрузки: 2017-09-24
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0.29/5
...) for Science and Technology Satellite (STSAT)-2C as one of ILRS prediction... history of KAS CPFs for STSAT-2C generation is summarized. We will... the Science and Technology Satellite (STSAT)-2C as one of ILRS prediction... Consolidated Prediction Format (CPF). The STSAT-2C is the first Korean satellite... main provider of CPFs for STSAT-2C is the Korea Advanced Institute... center consistently provides CPFs for STSAT-2C. However, KAI CPFs based on... for orbit determination (OD) for STSAT-2C is SLR observations, and therefore... Albedo pressure Empirical acceleration GGM-2C (200 by 200) [5] JPL DE... < 1 cm), new KAS CPF for STSAT-2C is generated. Overall process of... operation. The SLR tracking for STSAT-2C are very few and sparse... (3,526 NPs), and however, for STSAT-2C, the only 204 passes (2,215... process for CPFs generation for STSAT-2C has two steps. The first... the condition for OD for STSAT-2C is very poor, short/sparse... small (under 6), the OD for STSAT-2C cannot be performed. For reliable... of 35 KAS CPFs for STSAT-2C were uploaded to CDDIS data... details of SLR observations for STSAT-2C and KAS CPFs follow-up... (KAS) provides supplementary CPFs for STSAT-2C using SLR observations. The proper... is accomplished, KAS CPFs for STSAT-2C can be generated. The unsolved... is to attempt to track STSAT-2C using KAS CPFs, however it... tracking for STSAT-2C. Acknowledgements The authors deeply appreciate the STSAT-2C mission operation... al., 2014. Operation results of STSAT-2C satellite. 2014 KSAS Spring Conference.... Orbit determination and analysis for STSAT-2C. 18th International Workshop on Laser...



Дата загрузки: 2017-09-24
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0.24/5
... Orbit determination and analysis for STSAT-2C Y.-R. Kim, E. Park, H.-C. Lim Korea Astronomy...) satellite, Science and Technology SATellite (STSAT)-2C was launched on January 30... Vehicle (KSLV)1. SLR tracking for STSAT-2C was started on March 29...) for STSAT-2C. In this study, OD using SLR measurements for STSAT-2C is... orbits for STSAT-2C. Introduction The Science and Technology SATellite (STSAT)-2C is the..., 2013. The primary mission of STSAT-2C is to develop spacecraft and.... The specification of STSAT-2C is displayed at Table 1. STSAT-2C has elliptical orbit.... Figure 1 shows the shape of STSAT-2C. The primary SLR application is... Laser Ranging Service (ILRS) supports STSAT-2C by global SLR tracking. First... 2013, 12 stations are tracking STSAT-2C by SLR. Changchun, Grasse, Graz... centers normally provide CPFs. For STSAT-2C, KAI (Korea Advanced Institute of..., 2013. However, the CPFs of STSAT-2C, which are predicted based on..., have low accuracy, and therefore STSAT-2C has bad observability for SLR... 2 shows the tracking history of STSAT-2C. In this figure, we can... more accurate orbit acquisition for STSAT-2C is getting more difficult. In... the OD using SLR for STSAT-2C to make enhanced orbit. For... confirmation. Table 1. Mission parameters of STSAT-2C Parameter Sponsor Primary applications Primary... 0.082 300 1500 100 Figure 1. STSAT-2C satellite (http://ilrs.gsfc.nasa... 2. Current ILRS tracking statistics of STSAT-2C (2013/10) Station Name Changchun... 255 Figure 2. Tracking history of STSAT-2C measurements. Orbit determination using SLR..., the configurations of OD for STSAT-2C are summarized. For OD, NASA... 3. Dynamic and measurement models for STSAT-2C orbit determination Model Earth gravity...) Table 4. The summary of selected STSAT-2C arcs Arc 1 2 3 Start Time 05... The condition for OD of STSAT-2C is poor, and therefore it... 5. The post-fit residuals of STSAT-2C orbit determination Arc 1 2 3 Day 0501... (OD) using SLR measurements for STSAT-2C. The NASA/GSFC GEODYN II... reliability confirmation. The OD for STSAT-2C shows the typical results in... tracking and precise orbits for STSAT-2C. References Altamimi, Z., Collilieux, X., Legrand, J., Garayt...



Дата загрузки: 2017-06-15
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0.09/5
... (A&B) P4.1 Time bias analysis of STSAT-2C orbit predictions Y.-R. Kim, E. Park, D. Kucharski... (A&B) P4.1 Time bias analysis of STSAT-2C orbit predictions Y.-R. Kim(1), E. Park(1), D. Kucharski... The Science and Technology Satellite (STSAT)-2C is the first Korean satellite... and Space Science Institute. Because STSAT-2C has no GPS receiver and... for successful SLR tracking for STSAT-2C. The quality check of orbit.... Because SLR normal points of STSAT-2C have very sparse distribution, different... for STSAT-2C and discusses a strategy for reducing time biases of STSAT-2C orbit...



Дата загрузки: 2017-03-28
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0.06/5
... the Science and Technology Satellite (STsat) program in the 2000s, while... into KARI’s Science Technology Satellite-1 (STsat-1) project though SaTReC did actual...). (in Korean) 397 “Independent Launching STsat-2 by 2005,” Yeonhap News, (September...), four science and technology satellites (STsat-series) and two geostationary satellites... with the KOMPsat and KITsat/STsat program since 1990s, yet the... payload of KSLV-1, SaTReC developed STsat-2 (Science and Technology Satellite-2) in... to KITsat-4, also known as STsat-1, in orbit since September 2003.436 The 100-kilogram satellite STsat-2 would carry two main payloads... precise orbit information of the STsat-2. During the two years spent...-2(1993), KITSAT-3(1999), and KITsat-4/STsat-1(2003). See Chapter 3 of this...., “Exploring Space on a Small Satellite, STSat-2: A Test Bed for New Technologies... 2009,440 blasted off with STsat-2A at the Naro Space... a payload of STsat-2B that was identical to STsat-2A took place... off smoothly and placed the STsat-2C into orbit. The Korean government... KITsat-3 and KOREAsat-3 (1999), KITsat-4/STsat-1(2003), MBsat (2004), KOMPsat-2 and... COMS-1 (2010), KOMPsat-3 (2012), STsat-2c, KOMPsat-5, and STsat-3 (2013), and KOMPsat-3A... international competitiveness in space technology. STsat is devoted to preliminary research..., KOMPsat series), Satellites (KOMPsat, KoreaSat, STsat, COMSat series), Sounding Rockets (KSRIII.... “Exploring Space on a Small Satellite, STSat-2: A Test Bed for New Technologies...



Дата загрузки: 2017-09-24
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0.36/5
A STATUS REPORT ON KASI PREDICTION CENTER (KAS). Y.-R. Kim, E. Park, and H.-C. Lim, Center for Space Situational Awareness, Korea Astronomy and Space Science Institute, 776, Daedeok-Daero, Yuseong-gu, Daejeon, 305-348, South Korea, yrockkim@kasi.re.kr. Introduction: The Korea Astronomy and Space Science Institute (KASI) has been providing a supplementary Consolidated Prediction Format (CPF) for STSAT-2C as one of ILRS prediction centers since April 7, 2014. The STSAT-2C is the first Korean satellite equipped with the laser retro-reflector array for satellite laser ranging (SLR). The abbreviation in CPF files is KAS. The main provider of CPFs for STSAT2C is the Korea Advanced Institute of Science and Technology (KAIST, KAI). The KAI prediction center consistently provides CPFs for STSAT-2C. However, KAI CPFs based on two line element (TLE) have limits in ensuring accuracy. The only source for orbit determination (OD) for STSAT-2C is SLR observations, and therefore an attempt to make enhanced CPFs from SLR-based OD was accomplished and KASI started to operate KAS prediction center. Operation Status: The operation of KAS prediction center has two stages: test period and regular period. The SLR trackings for STSAT-2C are very few, for example, in April 2014, the only 19 passes during 9 day were uploaded to EDC data center. Therefore, daily CPFs were generated by using OD and their prediction results during from 7 to 22 April, 2014. As a result, only SLR-based CPFs from OD with new SLR observations have meaningful accuracy. In regular period, from 28 April to now, 2014, only if new SLR trackings are added, OD and CPFs generation are tried. Finally, a total of 31 KAS CPFs for STSAT-2C were uploaded to CDDIS data center as of September 17, 2014. Prediction Procedure: The process for CPFs generation for STSAT-2C has two steps. First is OD for STSAT-2C using NASA/GSFC GEODYN II software. Because the condition for OD for STSAT-2C is very poor, short/sparse measurements and inaccurate initial orbit information, the successful estimation is a lot of hard work. If the number of SLR normal points is small (under 6), the OD for STSAT-2C cannot be performed. The information of initial orbit can be obtained from KAI CPFs. Second is to generate CPFs from OD results. After OD, predicted orbits based on determined orbits can be transformed to geocentric true body fixed reference frame, which is a default frame of CPFs. Finally, generated SLR-based CPFs can be compared to KAI CPFs for consistency verification and uploaded to CDDIS data center. Figure 1 shows the flowchart of KAS CPFs for STSAT2C generation. Figure 1. The flowchart of KAS CPFs Generation Conclusions and Future Works: The KASI prediction centers (KAS) provides CPFs for STSAT-2C. If SLR tracking is accomplished, KAS CPFs for STSAT-2C can be generated. The unsolved issue is to confirmed the practical accuracy of KAS CPFs. Now, the only way to assess KAS CPFs accuracy is to track STSAT-2C using KAS CPFs, however it is not easy work because satisfying all condition such as CPFs, SLR NPs, day time and weather at the same time is very hard. We will prepare better strategy for quality assessment of KAS CPFs and continuously try to generate confirmed CPFs for more SLR tracking for STSAT-2C. References: [1] Kim Y.-R., Park E., and Lim H.-Y. (2013) 18th International Workshop on Laser Ranging.



Дата загрузки: 2017-04-23
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0.03/5
... and EVA Systems Oranim 3-A A3.2C Moon Exploration – Part 3 Schwartz Hall... Hall ASSOCIATED PROGRAMMES & EVENTS A3.2C Moon Exploration – Part 3 Fri, 16..., The Netherlands CONFERENCE PROGRAMME A3.2C. Moon Exploration – Part 3 October 16..., United States; IAC-15.A3.2C.1 STUDENTS & YOUNG PROFESSIONALS EVENTS OPTIMAL... (ISRO), India IAC-15.A3.2C.2 POLYGONAL-LIKE PERIODIC ORBIT AND... Liang, , China IAC-15.A3.2C.3 ASSOCIATED PROGRAMMES & EVENTS NAVIGATION OF... Liu, , China IAC-15.A3.2C.12 (withdrawn) ASSESSMENT OF THE... Fonseca, , Brazil IAC-15.A3.2C.13 THE FORMATION AND EVOLUTION... Zhong, , China IAC-15.A3.2C.14 (withdrawn) AUTONOMOUS LUNAR ORBIT... Aerospace, China IAC-15.A3.2C.15 TWO-SEGMENT LUNAR FREE... Aerospace, China IAC-15.A3.2C.16 PLANETARY SURFACE MODELLING AND... — Schwartz Hall IAC-15.A3.2C.5 IAC-15.A3.3A.1 EXHIBITION... & Technical TOURS IAC-15.A3.2C.6 ANALYSIS OF MANNED LUNAR ROVERS... Qiu, China IAC-15.A3.2C.7 AUTHORS’ INDEX DYNAMICS OF WEAK... MESSAGES ORGANISERS IAC-15.A3.2C.11 CONCEPTUAL DESIGN OF A RECONFIGURABLE..., United States; IAC-15.A3.2C.4 (withdrawn) IAC-15.A3.3B... Technical Programme IAC-15.A3.2C.10 COMMERCIAL PARTNERSHIP TO ADVANCE... PROGRAMMES & EVENTS IAC-15.A3.2C.9 IAC-15.A3.3A.5 IAC... & Technical TOURS IAC-15.A3.2C.8 ADVANCES IN THE HARDWARE/SOFTWARE... VIBRATION COMPONENT TEST SPECIFICATION FOR STSAT (SCIENCE AND TECHNOLOGY SATELLITE) Talgat...), United Kingdom IAC-15.D1.5.2 STSAT-2C MISSION ACHIEVEMENTS WITH ON ORBIT...-15.A6.4.9 IAC-15.A3.2C.7 IAC-15.B1.3.9 IAC-15....4.1 IAC-15.A3.2C.14 IAC-15.A3.2C.15 IAC-15....IP.11 IAC-15.A3.2C.4 IAC-15.D4.1.8 CA CA....E1.7.11 IAC-15.A3.2C.8 IAC-15.C4.1.6 IAC-15...-15.D2.6.5 IAC-15.A3.2C.7 IAC-15.D3.3.7 IAC-15...-15.A3.2C.4 IAC-15.A3.2C.5 IAC-15.A3.2C.6 IAC-15...-15.B4.2.5 IAC-15.A3.2C.12 IAC-15.A3.IP....A5.3-B3.6.3 IAC-15.A3.2C.7 IAC-15.D2.8-A5.4.6 IAC...-15.A1.4.3 IAC-15.A3.2C.12 IAC-15.A3.3B...-15.E3.3.6 IAC-15.A3.2C.3 IAC-15.A1.2.5 IAC-15....B1.4.6 IAC-15.A3.2C.5 IAC-15.A3.2C.6 IAC-15.C3....A6.IP.6 IAC-15.A3.2C.10 IAC-15.A1.3.8 IAC....A3.2A.3 IAC-15.A3.2C.10 IAC-15.C4.IP...-15.A7.3.5 IAC-15.A3.2C.9 IAC-15.B2.3.12 IAC...-15.E1.7.6 IAC-15.A3.2C.1 IAC-15.C2.1.2 IAC-15....IP.11 IAC-15.A3.2C.4 IAC-15.E4.2.7 IAC-15.A2.6.3 IAC-15.A3.2C.4 IAC-15.B2.6.12 IAC...-15.B2.6.9 IAC-15.A3.2C.16 IAC-15.A6.IP....IP.21 IAC-15.A3.2C.2 IAC-15.A6.IP.4 IAC...-15.A3.2C.4 IAC-15.A3.2C.5 IAC-15.A3.2C.6 IAC-15...-15.A1.5.9 IAC-15.A3.2C.10 IAC-15.C2.IP....1.8 IAC-15.A3.2C.14 IAC-15.A3.2C.15 IAC-15....47 IAC-15.A3.2C.5 IAC-15.A3.2C.6 IAC-15.D5...-15.C2.2.3 IAC-15.A3.2C.4 IAC-15.B6.3.13 IAC...-15.C4.6.6 IAC-15.A3.2C.11 IAC-15.C2.IP...-15.C2.7.4 IAC-15.A3.2C.3 IAC-15.D1.1.6 IAC-15...-15.B4.8.4 IAC-15.A3.2C.1 IAC-15.E3.1.10 IAC....IP.8 IAC-15.A3.2C.5 IAC-15.A3.2C.6 IAC-15.B6...-15.C2.7.4 IAC-15.A3.2C.10 IAC-15.D1.6.12...-15.B4.3.1 IAC-15.A3.2C.3 IAC-15.E2.4.5 IAC-15...-15.E5.4.3 IAC-15.A3.2C.8 IAC-15.E1.8.2 IAC-15...-15.A4.1.1 IAC-15.A3.2C.11 IAC-15.A1.5.6 IAC....4.9 IAC-15.A3.2C.14 IAC-15.A3.2C.15 IAC-15....C2.7.4 IAC-15.A3.2C.6 IAC-15.A3.2C.5 IAC-15.A3...-15.D2.3.6 IAC-15.A3.2C.2 IAC-15.C1.8.7 IAC-15....C1.IP.6 IAC-15.A3.2C.2 IAC-15.D6.1.2 IAC-15....A3.2A.3 IAC-15.A3.2C.10 IAC-15.A2.2.10...-15.C3.3.7 IAC-15.A3.2C.13 IAC-15.D1.7.4 IAC...



Дата загрузки: 2016-11-02
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0.04/5
....04.1992 Francia COM TELECOM 2C 06.12.1995 Francia COM...ñado del satélite INSAT 2C. Pesaba 2.283 Kg. Fue enviado... Japón COM Japón COM BSAT 2C BSAT 3A 11.06.2003... satélites SJ 2B y SJ 2C. Pesaba 483 Kg y medía 1,1 m de... satélites SJ 2A y SJ 2C. Pesaba 257 Kg y constaba de...ósfera. Cayó sobre la SJ-2C 19.09.1981 China EXP... Jiuquan con un cohete CZ-2C. La órbita es una de... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita polar... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita polar... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita polar... Jiuquan con un cohete CZ-2C. El cohete falló en una... Taiyuan con un cohete CZ-2C que también llevaba otro sat... Taiyuan con un cohete CZ-2C que también llevaba otro sat... Jiuquan con un cohete CZ-2C. Destinado a una órbita polar heliosincr... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita heliosincr... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita heliosincr... Jiuquan con un cohete CZ-2C. Fue enviado a una órbita heliosincr... Jiuquan con un cohete CZ-2C. Fracasó al explotar a los 20... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 1.700 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.400 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Pesaba 2.500 Kg. Fue enviado... Jiuquan con un cohete CZ-2C junto al satélite Freia... Jiuquan con un cohete CZ-2C. Pesaba 2.099 Kg. Fue enviado... Jiuquan con un cohete CZ-2C. Destinado a estudios sobre la microgravedad..., GMT, con un cohete CZ-2C en la base de Jiuquan....05.2002 China MET FY-2C 19.10.2004 China MET...-024B. También llamado Feng Yun-2C. Satélite meteorológico, primero...ón. Destinado a sustituir al antiguo FY-2C. Su número COSPAR es 2008... años. También llamado ZX-2C y Chinasat-2C. Satélite de telecomunicaciones posiblemente... prevista de 15 años. ZHONGXING 2C 03.11.2015 China MIL... Taiyuan con un cohete CZ-2C. Quedó en órbita heliosincrónica... Xichang con un cohete CZ-2C que también llevaba al sat... Naxing 1 con un cohete CZ-2C a las 23 h 59 m, hora local... Xichang con un cohete CZ-2C que también llevaba al sat... Xichang con un cohete CZ-2C. Estuvo en una órbita de... y 97,99º de inclinación. ZY-2C 06.11.2004 China MIL... Taiyuan con un cohete CZ-2C. Su órbita fue una polar... Taiyuan con un cohete CZ-2C. Fue enviado a una órbita polar... Taiyuan con un cohete CZ-2C. Fue enviado a una órbita polar... Taiyuan con un cohete CZ-2C. Fue enviado a una órbita heliosincr... Taiyuan con un cohete CZ-2C-SMA que también llevaba otro... Taiyuan con un cohete CZ-2C-SMA que también llevaba otro... Taiyuan con un cohete CZ-2C que también llevaba otros 3 sat... Taiyuan con un cohete CZ-2C que también llevaba otros 3 sat... Taiyuan con un cohete CZ-2C que también llevaba otros 3 sat... Taiyuan con un cohete CZ-2C que también llevaba otros 3 sat... órbita polar heliosincrónica. XW-2C 19.09.2015 China COM....07.1993 India COM INSAT 2C 06.12.1995 India COM... compañía del satélite TELECOM 2C. Pesaba 2.050 Kg. Su órbita... y estaba destinado a suplantar a los INSTA 2C y 2D. Fue enviado a una órbita... 5), que también llevaba al BSAT-2C japonés, hacia una órbita geoestacionaria... chinos con un cohete CZ-2C en Jiuquan junto al sat....2015 Corea del Sur REC STSAT KAISTSAT-4 200327.09.2003 Corea... CIE AST STSAT-2 25.08.2009 Corea del Sur CIE STSAT-2B 10.06.2010 Corea del Sur CIE STSAT-2C 30... Corea del Sur. También llamado STSAT-1 y URIBYOL-4. Satélite astronómico...). Vida útil proyectada de 2 años. STSAT-3 21.11.2013 Corea del....12.2000 ASTRA COM ASTRA 2C 16.06.2001 ASTRA COM... Este. Destinado a sustituir al ASTRA 2C. Vida útil prevista de 15... Taiyuan con un cohete CZ-2C. Su órbita tenía un perigeo... Taiyuan con un cohete CZ-2C. Su órbita tenía un perigeo... GMT con un cohete CZ-2C/SD en Taiyuan junto al... GMT con un cohete CZ-2C/SD en Taiyuan junto al... GMT con un cohete CZ-2C/SD en Taiyuan junto al... GMT con un cohete CZ-2C/SD en Taiyuan junto al... Taiyuan con un cohete CZ-2C. Pesaba 689 Kg. Construido por... Taiyuan con un cohete CZ-2C. Pesaba 689 Kg. Construido por... Taiyuan con un cohete CZ-2C. Pesaba 689 Kg. Estuvo en... Taiyuan con un cohete CZ-2C. Pesaba 689 Kg. Estuvo en... Taiyuan con un cohete CZ-2C. Estuvo en una órbita de... Taiyuan con un cohete CZ-2C. Estuvo en una órbita de... Xichang con un cohete CZ-2C, primero de tal modelo lanzado... Taiyuan con un cohete CZ-2C. Peso 243 Kg y lleva 8 instrumentos...



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... 2012, Science and Technology Satellite-2C (STSAT-2C) will be launched by Korea... laser oscillator and other technologies, STSAT-2C aims to demonstrate the operation... the Science and Technology Satellite-3 (STSAT-3) with a hyper-spectral camera and... series, which is the subsequent STSAT space programme to demonstrate the...) in an elliptical orbit. With STSAT-2C, KSLV-1 is to be launched...