Research Article

A Spherical Micro Satellite Design and Detection Method for Upper Atmospheric Density Estimation

Table 1

Simulation conditions.

Simulation time (s)Initial orbital element
Orbital height (km)
EccentricityInclination (°)Right ascension of ascending node (°)Argument of perigee (°)True anomaly (°)

1500412.18096.8213340.25100
512.18096.8213340.25100
612.18096.8213340.25100