The Long March 2D, also known as the Chang Zheng 2D, CZ-2D and LM-2D, is a Chinese orbital carrier rocket. It is a 2-stage carrier rocket mainly used for launching LEO and SSO satellites.
The China Aerospace Science and Technology Corporation (CASC) is the main contractor for the Chinese space program. It is state-owned and has a number of subordinate entities which design, develop and manufacture a range of spacecraft, launch vehicles, strategic and tactical missile systems, and ground equipment. It was officially established in July 1999 as part of a Chinese government reform drive, having previously been one part of the former China Aerospace Corporation. Various incarnations of the program date back to 1956.
Shijian 19 is a Chinese recoverable satellite for hoisting various scientific experiments in microgravity. Unlike previous similar Chinese satellites, the return capsule can be reused up to 15 times and can carry about 500 kg of recoverable payload, as well as 200 kg of unrecoverable payload. This type of satellite can be flown in a short term configuration powered by batteries or in a long term configuration with solar arrays.
Low Earth OrbitThe Yunhai-1 satellite is designed for detecting environmental elements in the atmosphere and ocean, the space environment, disaster prevention and reduction, and scientific experimentation. It is made by the Shanghai Institute of Spaceflight Technology.
Sun-Synchronous OrbitThis launch carries multiple payloads, including 6 new satellites for the Jilin-1 commercial Earth observation satellite constellation and Qilu-2/3, 2 optical Earth observation satellites for the Shandong Province Industrial Technology Research Institute.
Sun-Synchronous OrbitGaofen-5-01A is a hyperspectral Earth observation satellite. Instruments include a 1500 km swath width Infared imager, a 2.5nm spectral-resolution visible-near infrared hyperspectral imager & a differential absorption spectrometer for measuring atmospheric trace gas.
Sun-Synchronous OrbitASO-S (Advanced Space-borne Solar Observatory) is a Chinese solar space observatory that aims to study the interaction between the Sun's magnetic field, solar flares and coronal mass ejections. It's the first space solar observatory of China. ASO-S is a 3-axis stabilized satellite with a mass of less than 1,000 kg with a pointing accuracy of 0.01° and an orientation stability of 1 to 2 arc seconds every 20 seconds. The payload has a mass below 335 kg and consumes about 300 watts. The platform's pointing accuracy is lower than 0.01°, the measurement accuracy is lower than 1 arc second and the orientation drift is below 0.0004°/s. ASO-S has three instruments: - The Full-Disc Vector Magnetograph (FMG) instrument is intended to map the magnetic field of the photosphere over the entire solar disk. It includes an imager, an optical polarization system and a CCD detector. - The Hard X-ray Imager (HXI) camera should image the whole solar disk in X-rays. The instrument is optimized to take images of solar flares. - A set of three LST (Lyman-alpha Solar Telescope) telescopes is used to observe the Lyman-alpha line (121.6 nm) of solar flares up to a distance of several solar radii from the Sun's disk. These three telescopes are SDI (to obtain an image of the solar disk), SCI (coronagraph for observation between 1.1 and 2.5 solar radii) and WST (white light emitted by the solar disk used for calibration purposes).
Sun-Synchronous OrbitThe Yunhai-1 satellite is designed for detecting environmental elements in the atmosphere and ocean, the space environment, disaster prevention and reduction, and scientific experimentation. It is made by the Shanghai Institute of Spaceflight Technology.
Sun-Synchronous OrbitXihe, also known as the Chinese Hα Solar Explorer (CHASE), is designed to test a newly developed satellite platform and conduct solar observations. The scientific payload of the satellite is an Hα imaging spectrograph (HIS), which can, for the first time, acquire full-disk spectroscopic solar observations in the Hα waveband. It will complement the observations by on-orbit solar spacecraft (such as SDO, IRIS, STEREO and PSP), as well as future solar missions of the Solar Orbiter and the Chinese Advanced Space-based Solar Observatory (ASO-S). Mission is named Xihe after a solar deity from Chinese mythology.
Sun-Synchronous OrbitTH 1 (Tianhui-1 = "Sky drawing") is a Chinese stereo-topographic mapping satellite operated by the People’s Liberation Army (PLA). The satellites are built by the Hangtian Dongfanghong Weixing Corporation and the China Aerospace Science and Technology Corporation and the Chinese Academy of Space Technology (CAST). The satellites operate on a 500 km circular sun synchronous orbit. Electrical power is provided by two deployable solar panels that is stored on onboard batteries. They are equipped with a three-dimensional survey camera and a CCD camera with a ground resolution of 5 meters, spectral region of 0.51 µm to 0.69 µm and with a camera angle of 25 degrees. Also on board is a multi-spectral camera with a ground resolution of 10 meters operating in four spectral bands of 0.43 µm to 0.52 µm, 0.52 µm to 0.61 µm, 0.61 µm to 0.69 µm, and 0.76 µm to 0.90 µm. The swath width of the cameras is 60 kilometers wide.
Sun-Synchronous OrbitGaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms.
Sun-Synchronous OrbitGaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms.
Sun-Synchronous OrbitGaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms.
Sun-Synchronous OrbitGaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms.
Sun-Synchronous OrbitThe Yunhai-1 satellite is designed for detecting environmental elements in the atmosphere and ocean, the space environment, disaster prevention and reduction, and scientific experimentation. It is made by the Shanghai Institute of Spaceflight Technology.
Shiyan 6 is the main payload of the launch and is reported to be used for "space environment measurements and related technical tests". It was launched along with 4 small satellites, among which are a China's first privately designed low Earth orbit communications satellite Jiading-1 and China's first software-based satellite Tianzhi-1.
Low Earth OrbitGaofen is a series of civilian Earth observation satellites developed and launched for the China High-definition Earth Observation System (CHEOS), a state-sponsored programme aimed to develop a near-real time, all-weather, global surveillance network consisting of satellite, near-space (stratosphere) airships, and aerial observation platforms. Luojia-1 is a 6U Earth observation cubesat prototype.
Sun-Synchronous OrbitZhangheng-1, also known as CSES (China Seismo-Electromagnetic Satellite) is a scientific mission dedicated to studying the ionospheric precursors of earthquakes. Data collected by the mission will also allow studying solar-terrestrial interactions and phenomena of solar physics. This mission is a collaboration between China National Space Administration and the Italian Space Agency. CSES satellite weighs about 730 kg and it is to reside in a 98° sun-synchronous circular orbit at an altitude about 500 km, where it is expected to operate for 5 years.
Sun-Synchronous OrbitThese two satellites, also known as SuperView-2 constellation, are remote sensing satellites to operate in a 500 km sun-synchronous orbit. This is a second pair of such satellites to be launched for the SuperView company. They are capable of providing imagery with 0.5 m panchromatic resolution and 2 m multispectral resolution.
Sun-Synchronous OrbitVRSS-2 is the second Venezuelan remote sensing satellite. Spacecraft was built by China. Weighing about 1000 kg, it is to operate in sun-synchronous orbit at an altitude of 645 kilometres, providing services in traffic management, disaster warning and prevention, tracking agriculture and land use.
Sun-Synchronous OrbitTansat is a global CO2 (Carbon Dioxide) monitoring scientific experiment satellite and demonstration mission. The main components of the project are: The global carbon dioxide monitoring platform. A high spectral and spatial resolution CO2 detector. A multispectral cloud and aerosol detector. And a ground data processing and inversion CO2 verification system.
Low Earth OrbitThe Yunhai-1 satellite is designed for detecting environmental elements in the atmosphere and ocean, the space environment, disaster prevention and reduction, and scientific experimentation. It is made by the Shanghai Institute of Spaceflight Technology.
Sun-Synchronous OrbitQuantum Experiments at Space Scale (QUESS) is the first satellite purpose-built for quantum experiments in the world. The 600kg satellite will test long range quantum communications at longer range than ever before. So far scientists have managed to reach up to around 300km, but they hope that in space the range can be increased significantly. They will be testing it up to around 1200km. The mission is expected to last 2 years
Sun-Synchronous OrbitShijian-10 is a retrievable satellite that will perform 19 experiments in low earth orbit over 15 days before returning to earth. The experiments onboard include the Soret Coefficient in Crude Oil (SCCO) experiments, as well as experiments on radiation, combustion, and biology. Due to the short lifespan and retrievable design the craft will not be encapsulated within a fairing and will be powered by chemical batteries instead of solar panels.
Low Earth Orbit