Electromagnetic Doppler Shift Data for Satellites in Circular Polar Orbits at Altitudes Between 250 and 1000 Nautical Miles
Abstract
A computer program has been used to generate doppler shift of an electromagnetic signal from an orbiting satellite as a function of time. The predicted doppler shift as a function of time is available in two different output formats: a continuous plot of doppler as a function of time before and after closest approach and a tabulated list of doppler as a function of time. The computer program employs a spherical earth and a circular, polar orbit for the satellite.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1966
- Accession Number
- AD0640606
Entities
People
- Gary N. Matuck
- John F. Clark
Organizations
- Johns Hopkins University