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What information is included in the Mission Awareness CSV?

Explore the access opportunity metadata fields included in Capella’s Mission Awareness CSV to support repeat task planning.

Users can leverage the Mission Awareness tool to understand potential satellite access opportunities for a specific task and plan the cadence of a repeat task. The Mission Awareness tool generates a Comma Separate Value (CSV) file with the list of potential satellite access times and the associated metadata.  

Column Name

Description

Unit

Center WGS84

Point object for the center point of the access opportunity in the WGS84 coordinate system.

Point

Center ECEF

Point object for the center point of the access opportunity in the Earth-centered, Earth-fixed (ECEF) coordinate system.

Point

Spacecraft ID

Capella spacecraft set to perform collection.

Number

Access ID

A unique identifier for a potential satellite access time.

String

Access Request ID

A unique identifier for the submission to Mission Awareness.

String

Window Open

Earliest time when acquisition can occur. Image acquisition can begin any time after the Window Open time up to the Window Close time.

Datetime

Window Close

Latest time when acquisition can occur. Image acquisition can begin any time after the Window Open time up to the Window Close time.

Datetime

Orbital Plane

The regular, repeating path of the spacecraft around the Earth. Capella spacecrafts are in mid-latitude (47 degrees and 53 degrees) orbits.

Number

Orbit State

Whether the spacecraft is on the Ascending (South to North) or Descending (North to South) orbit during image acquisition.

String

Look Direction

Whether the spacecraft is looking Left or right with respect to its velocity vector during image acquisition.

String

Local Mean Time

Local time at center of access opportunity in astronomical time (seconds).

Number [Seconds]

Az Open

Counterclockwise angle with respect to the azimuth open in the topocentric geodetic ENZ coordinate system.

Number

Az Close

Counterclockwise angle with respect to the azimuth close in the topocentric geodetic ENZ coordinate system.

Number

Elev Min

Minimum angle between the tangent to the surface and the line of sight of the satellite as seen from center point during the access window. 

Number

Elev Max

Maximum angle between the tangent to the surface and the line of sight of the satellite as seen from center point during the access window. 

Number

Off-Nadir Min

Minimum look angle between the spacecraft’s nadir position and the SAR beam in degrees.

Number [Degrees]

Off-Nadir Max

Maximum look angle between the spacecraft’s nadir position and the SAR beam in degrees.

Number [Degrees