NEDM2020: ionosphere electron density
Last modified at Aug 12th, 2024, 12:00 GMT
Description
The Neustrelitz Electron Density Model NEDM2020 can provide electron concentration at any given location and time in the ionosphere for trans-ionospheric applications (altitude range 80 – 20,000 km) based on user latitude, longitude, height, day of year, and universal time as inputs, with driving parameter F10.7. The empirical model is an amalgamation of altitude region specialized approaches for the plasmasphere, F layer, and E layer.
Capabilities
-
Ionosphere electron density
- Observed Property
- Dimensionality Instance
- Units
Data Levels
Further Information and Resources
Resources
More Properties
Property | Value |
---|---|
Algorithm | Not used |
Name (from Processing Input (1/8) > Input Output) | F10.7 solar flux [sfu] (optional) |
Character String (from Processing Input (1/8) > Input Output > Description > LE Source > Description) | F10.7 in solar flux units. This value is optional: Not setting it will instruct the server to try and fetch the F10.7 value for the given datetime automatically. |
Name (from Processing Input (2/8) > Input Output) | Receiver altitude [km] |
Character String (from Processing Input (2/8) > Input Output > Description > LE Source > Description) | Altitude of the receiver in kilometers. |
Name (from Processing Input (3/8) > Input Output) | Receiver latitude [deg] |
Character String (from Processing Input (3/8) > Input Output > Description > LE Source > Description) | Latitude of the receiver in degrees (signed decimal number). |
Name (from Processing Input (4/8) > Input Output) | Receiver longitude [deg] |
Character String (from Processing Input (4/8) > Input Output > Description > LE Source > Description) | Longitude of the receiver in degrees (signed decimal number). |
Name (from Processing Input (5/8) > Input Output) | Satellite altitude [km] |
Character String (from Processing Input (5/8) > Input Output > Description > LE Source > Description) | Altitude of the satellite in kilometers. |
Name (from Processing Input (6/8) > Input Output) | Satellite latitude [deg] |
Character String (from Processing Input (6/8) > Input Output > Description > LE Source > Description) | Latitude of the satellite in degrees (signed decimal number). |
Name (from Processing Input (7/8) > Input Output) | Satellite longitude [deg] |
Character String (from Processing Input (7/8) > Input Output > Description > LE Source > Description) | Longitude of the satellite in degrees (signed decimal number). |
Name (from Processing Input (8/8) > Input Output) | Date-Time [ISO] |
Character String (from Processing Input (8/8) > Input Output > Description > LE Source > Description) | Date and time of interest given as an ISO 8601 compliant string. |
Software Reference | Not used |
Editor | German Aerospace Center - DLR - Institute for Solar-Terrestrial Physics |
Version | 1 |
Created | Monday 12th Aug. 2024, 12:00 |
Last Modified | Monday 12th Aug. 2024, 12:00 |