Computation of Satellite Position


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Documentation for package ‘asteRisk’ version 1.0.0

Help Pages

ECEFtoGCRF Convert coordinates from ECEF to GCRF
ECEFtoLATLON Convert coordinates from ECEF to geodetic latitude, longitude and altitude
ECItoKOE Calculate ECI coordinates from Keplerian orbital elements
GCRFtoECEF Convert coordinates from GCRF to ECEF
GCRFtoLATLON Convert coordinates from GCRF to geodetic latitude, longitude and altitude
getLatestSpaceData Retrieves the latest space data
hpop High-precision numerical orbital propagator
KOEtoECI Calculate ECI coordinates from Keplerian orbital elements
parseTLElines Parse the lines of a TLE
readTLE Read a TLE file
sdp4 Propagate an orbital state vector with the SDP4 model
sgdp4 Propagate an orbital state vector with the SGP4/SDP4 model
sgp4 Propagate an orbital state vector with the SGP4 model
TEMEtoECEF Convert coordinates from TEME to ECEF
TEMEtoGCRF Convert coordinates from TEME to GCRF
TEMEtoLATLON Convert coordinates from TEME to geodetic latitude, longitude and altitude