Payloads | Physical parameter | Specification |
Search coil magnetometer | 3 components of magnetic field | 10Hz-20kHz |
Electric field detector | 3 components of electric field | DC-3.5MHz |
Fluxgate magnetometer | 3 components of basic magnetic field | DC-10Hz |
GPS receiver | Ionospheric TEC | |
Plasma Analysis | Ion density Ion temperature Ion components Ion velocity | 102~107cm-3 500~5000K |
Langmuir probe | Electron density Electron temperature | 5×102~5×106cm-3 500~10000K |
Energetic Particle Detector | Proton flux Electron flux | 1.5MeV~200MeV ≧100keV |
Overhause Magnetometer | The total magnetic field intensity | 18000~65000nT |
Style of orbit | Circular polar orbit |
Altitude (Km) | 500 |
Inclination (deg) | ≧79° |
Period (min) | 97.3 |
Local time of descending node | 13:30pm |
Measurement precision of orbit | Real-time orbit determination: superior than:±100m Not real-time orbit determination: superior than ±50cm |
Attitude control(degree) | Pointing accuracy: ±0.5° Triaxial stability: ±0.1°/s (3σ) |
Revisiting period (day) | 5 |
Space between two orbit in a revisiting perod (longitude degree) | 5 |
17 Energetic electron flux variation around the Yushu earthquake on april 14, 2010
43 Particle precipitation caused by wave-particle gyroresonant interaction during NPM experiment
71 Introduction for China Seismo-Electromagnetic Satellite (CSES)・Constellation solution for temporal resolution
- Minimize the probability any EM disturbance is missed.
- In 2017, a 2-satellite constellation on 500km orbit is proposed for in situ observations.
・ Ionosphere plasma profile acquisition issue
-“Top Ionosphere Detector” equipment should be used at the top of ionosphere (Around 1000km).
- In 2020, a 2-satellite constellation is proposed for 1000km orbit.