
| 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.

