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New non-geosynchronous orbits for communications satellites to off-load daily peaks in geostationary trafficThe potential for satellites in two orbits, the sun-synchronous 12-hour equatorial orbit (STET) and the apogee at constant time-of-day equatorial orbit (ACE), to off-load peaks in the CONUS geostationary communications traffic is discussed. These orbits are found to require maneuvers of smaller magnitudes for insertion than geostationary orbits. Advantages of the ACE orbit over the STET orbit are discussed, including larger satellite mass capability for a given launch vehicle, lower slant ranges, and larger angular separation from the geostationary arc for a nonequatorial ground observer.
Document ID
19880023730
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Turner, A. E.
(Ford Aerospace and Communications Corp. Palo Alto, CA, United States)
Date Acquired
August 13, 2013
Publication Date
August 1, 1987
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 87-547
Accession Number
88A10957
Funding Number(s)
CONTRACT_GRANT: NAS3-24891
Distribution Limits
Public
Copyright
Other

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