orbit.Orbit: Timestamped orbital data for a satellite
timespan.TimeSpan: A series of timestamps.updater.getStoredEpochLimits: Returns limiting epochs for the stored TLEs for each sat in sat_id_list.updater.getTLEFilePaths: Fetch list of paths to TLE files.updater.updateTLEs: Fetch most recent TLE for provided list of satcat IDs.orbit: Class for orbital data.timespan: Class for series of timestamps.updater: Functions to update TLE of a satcat ID, and fetch where the file is stored.utilutil.celestrak: Functions to fetch TLEs from Celestrak.util.constants: Namespace of useful orbital constants.util.credentials: Functions to fetch and store spacetrack credentials on the system.util.elements_u: Utility functions for dealing with propagation element set strings.util.epoch_u: Utility functions for converting different epochs.util.exceptions: Generic exceptions that apply throughout satplot.util.orbital_u: Utility functions for orbital calculations.util.spacetrack: Functions to fetch TLEs from Spacetrack.orbit.Orbit: Timestamped orbital data for a satellite, coordinate system depending on the central body.orbit.OrbitAttrDict: A TypedDict providing type annotations for the Orbit class.timespan.TimeSpan: A series of timestamps.elements_u.ElementsLineDict: TypedDict container for lines of an element set.exceptions.DimensionError: Dimension of an array is invalid.exceptions.OutOfRangeError: The value is out of the acceptable range.spacetrack.InvalidCredentialsError: Error indicating invalid credentials used to access spacetrack.updater.getStoredEpochLimits: Returns limiting epochs for the stored TLEs for each sat in sat_id_list.updater.getTLEFilePaths: Fetch list of paths to TLE files.updater.updateTLEs: Fetch most recent TLE for provided list of satcat IDs.celestrak.getStoredEpochs: Return the start and end epoch for {sat_id}.temptle .celestrak.getTLEFilePath: Gives path to file where celestrak TLE is stored.celestrak.updateTLEs: Fetch most recent TLE for satcat IDs from celestrak.credentials.createCredentials: Script helper function to create and store credentials.credentials.fetchConfigCredentials: Fetch spacetrack credentials from config file.credentials.fetchKeyringCredentials: Fetch spacetrack credentials from system keyring.credentials.storeCredentials: Store spacetrack credentials in system keyring.elements_u.dictify3LEs: Turn list of strings into list of dicts storing TLE info.elements_u.split3LELineIntoFields: Create an ElementsLineDict from an element set line.elements_u.stringify3LEDict: Turn an element set dict 3LE dict back into a \n delimited string.epoch_u.datetime2TLEepoch: Converts a datetime to a TLE epoch string.epoch_u.datetime2sgp4epoch: Converts a datetime to an sgp4 epoch.epoch_u.epoch2datetime: Converts a fractional epoch string to a datetime object.epoch_u.epochEarlierThan: Check if epoch A is earlier than epoch B.epoch_u.epochLaterThan: Check if epoch A is later than epoch B.epoch_u.findClosestDatetimeIndices: Find the index of the closest datetime in source arr for each datetime in test_arr.epoch_u.getStoredEpochs: Return the start and end epoch for tle_path.orbital_u.calcMeanMotion: Returns mean motion [radians/s] for an elliptical or circular orbit with semi-major axis a.orbital_u.calcOrbitalVel: Return the instantaneous velocity magnitude for an elliptical orbit at position.orbital_u.calcPeriod: Returns the period of an elliptical or circular orbit.orbital_u.ssoInc: Generates required inclination for given altitude [km] to maintain Sun Syncrhonous orbit.spacetrack.doCredentialsExist: Checks if spacetrack credentials have been loaded into Spherapy.spacetrack.getStoredEpochs: Return the start and end epoch for {sat_id}.tle .spacetrack.getTLEFilePath: Gives path to file where spacetrack TLE is stored.spacetrack.updateTLEs: Fetch most recent TLE for satcat IDs from spacetrack.This file was automatically generated via lazydocs.