Systems and tagging interfaces for identification of space objects

A computer-implemented method for determining and displaying an orbit of an orbital object using observations of the orbital object, the method comprising:

• by an electronic processor configured to execute instructions stored in a non-transitory memory connected to the electronic processor:
• receiving, via an orbital object data interface, a plurality of sets of identifiers, wherein each set of identifiers corresponds to an orbital object;
• receiving, via a selection interface, a selection of a plurality of timepoints corresponding to the orbital object, wherein the selection of the plurality of timepoints comprises sets of identifiers within a display time period;
• determining an orbital path of the orbital object associated with the selected plurality of timepoints, wherein the orbital path is determined over an orbital time period that (i) overlaps the display time period, (ii) precedes the display time period, (iii) succeeds the display time period, or (iv) any combination thereof, the display time period spanning from a lower-time limit to an upper-time limit;
• and
• generating data configured to display a position-time graph comprising:
• a position axis spanning from a lower-position limit to an upper-position limit,
• a time axis spanning from the lower-time limit to the upper-time limit, and
• an indication of the orbital path spanning at least the first time period.

A computer-implemented method for displaying measurements of space objects, the method comprising:

• receiving, via an orbital object data interface, a plurality of sets of identifiers, wherein each set of identifiers corresponds to an orbital object
• receiving, via a selection interface, a track comprising a plurality of the sets of identifiers associated with the orbital object;
• generating data configured to display a position-time graph comprising:
• a position axis spanning from a lower-position limit to an upper-position limit,
• a time axis spanning from a lower-time limit to an upper-time limit;
• and
• a track representation comprising position-time points within the position-time graph, each of the plurality of position-time points corresponding to a set of identifiers having a time identifier of the plurality of sets of identifiers between the lower-time limit and the upper-time limit and having a position identifier of the plurality of sets of identifiers between the lower-position limit and the upper-position limit, wherein the track representation provides a view of at least a portion of the track;
• and
• in response to a user selection of the track and receipt of a user instruction to determine an orbit, generating updated data configured to display an orbit representation on the position-time graph by:
• determining an orbit of the orbital object using the selected track during a time period comprising a time after or before a current time;
• and
• overlaying the orbit representation corresponding to the determined orbit on the position-time graph.

A computer-implemented method for determining and displaying an orbit of an orbital object using observations of the orbital object, the method comprising:

• by an electronic processor configured to execute instructions stored in a non-transitory memory connected to the electronic processor:
• receiving, via an orbital object data interface, a plurality of sets of identifiers, wherein each set of identifiers corresponds to an orbital object;
• receiving, via a selection interface, a selection of a plurality of timepoints corresponding to the orbital object, wherein the selection of the plurality of timepoints comprises sets of identifiers within a time period associated with historical measurements;
• determining an orbital path of the orbital object associated with the selected plurality of timepoints, wherein the orbital path is determined over an orbital time period that (i) overlaps the time period associated with the historical measurements, (ii) precedes the display time period, (iii) succeeds the display time period, or (iv) any combination thereof, the orbital time period spanning from a lower-time limit to an upper-time limit;
• and
• generating a display interface having a position-time graph comprising:
• a position axis spanning from a lower-position limit to an upper-position limit,
• a time axis spanning from the lower-time limit to the upper-time limit, and
• an indication of the orbital path spanning at least the first time period.