1.1.2. General Options

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The simplest, but inefficient approach is “trial-and-error”, i.e., compare the time and location of all pairs of files within a given time window.

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A more sophisticated option is to use the observed orbital parameters (such as the Two Line Elements or TLE) with orbit prediction software such as Simplified General Perturbations Satellite Orbit Model 4 (SGP4). For instrument that has fixed or stable scan pattern such that the measurement time and location are determined by the satellite locations, this is very effective.

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Topic revision: r2 - 29 Oct 2009, AleksandarJelenak
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