TIME RELATIONS AND SHAPE VARIATION FOR THE GROUND TRACK OF 24-HOUR SATELLITE.
Abstract
The present study shows the time relation in describing sections of the ground track of a 24-hour satellite. The oscillation of an equatorial satellite is investigated and the dependence of the amplitude on eccentricity is shown. For elliptical inclined orbits the decrease of a lobe's size and its total disappearance are shown as functions of increasing eccentricity, of the perigee parameter and inclination. Plots illustrating typical cases are provided. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1968
- Accession Number
- AD0832510
Entities
People
- Peter Bielkowicz
Organizations
- Air Force Institute of Technology