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Table 1 Example of some parameters and estimated spacecraft potentials at the selected point shown as a pink cross in the right panel of Fig. 7

From: Development of space environment customized risk estimation for satellites (SECURES)

Long. [deg.] Lat. [deg.] Density [/cc] Temperature [keV] Pressure [nPa]
220.0  − 18.0 1.00 11.1 1.62
Eclipse = 1
Daylight = 0
Scientific satellite Commercial satellite
Surface potential Φsc[V] Surface potential ΦMAX [V] Frame potential ΦFRAME[V] Differential potential [V]
1  − 8700  − 5600  − 8100 2500
  1. This table is shown in the web viewer of the surface charging/ESD risk assessment system