Systems and visualization interfaces for identification and display of space object imagery

A system for displaying image data derived from photographs of space objects, the system comprising:

• a computer readable storage configured to communicate instructions for displaying image data derived from a plurality of photographs of space objects;
• a hardware processor in communication with the computer-readable storage, wherein the instructions, when executed by the hardware processor, are configured to cause the system to:
• receive image data derived from the plurality of photographs;
• derive a plurality of sets of identifiers, each of the sets associated with a photograph, wherein each set of identifiers corresponds to a space object and comprises:
• a name identifier;
• a time identifier;
• a latitude identifier;
• a longitude identifier;
• and
• a scalar identifier;
• automatically identify a first orbital object in at least one of the plurality of photographs;
• receive a user selection of a second orbital object not identified by the system in the at least one of the plurality of photographs;
• in response to the user selection of the second orbital object in the at least one of the plurality of photographs, derive a second set of identifiers corresponding to the second orbital object;
• in response to deriving the second set of identifiers corresponding to the second orbital object, automatically identify the second orbital object in a second photograph;
• in response to the user selection of the second orbital object within the at least one of the plurality of photographs, initiate a search for the second orbital object based on a plurality of identifiers associated with the first orbital object;
• determine a range of acceptable values associated with a boundary corresponding to a field of view shown in the at least one of the plurality of photographs;
• compare the derived second set of identifiers corresponding to the second orbital object with the plurality of identifiers associated with the first orbital object;
• determine that one or more identifiers corresponding to the second orbital object are within the range of acceptable values associated with the boundary;
• and
• display at least one of the derived second set of identifiers corresponding to the second orbital object.