This study note reviews the basic orbit parameters and characteristics of the four global navigation satellite constellations operational or planned in medium Earth orbit: GLONASS (Russia), GPS (USA), Beidou-M (China) and Galileo (Europe). The launch history, mission profile, spacecraft lifetime and maintenance strategy are detailed, based on the available literature and open information. The disposal rules applied so far to constellation spacecraft and upper stages are discussed, together with their long-term impact in terms of orbital evolution and possible crossing of the altitudes of the operational satellites. Moreover, the average cross section (randomly tumbling) is estimated for some of the spacecraft models of the constellations. Finally, the detailed input setup for the long-term simulations planned in the framework of the study is presented.

Review of medium earth orbit gnss constellation configuration, operation, maintenance and disposal

Anselmo L;Pardini C
2013

Abstract

This study note reviews the basic orbit parameters and characteristics of the four global navigation satellite constellations operational or planned in medium Earth orbit: GLONASS (Russia), GPS (USA), Beidou-M (China) and Galileo (Europe). The launch history, mission profile, spacecraft lifetime and maintenance strategy are detailed, based on the available literature and open information. The disposal rules applied so far to constellation spacecraft and upper stages are discussed, together with their long-term impact in terms of orbital evolution and possible crossing of the altitudes of the operational satellites. Moreover, the average cross section (randomly tumbling) is estimated for some of the spacecraft models of the constellations. Finally, the detailed input setup for the long-term simulations planned in the framework of the study is presented.
2013
Istituto di Scienza e Tecnologie dell'Informazione "Alessandro Faedo" - ISTI
Rapporto intermedio di progetto
Global navigation satellite systems
Medium earth orbits (MEO)
Configuration
Launch
Operations
Maintenance
Disposal
Spacecraft and rocket bodies characteristics
J.2 PHYSICAL SCIENCES AND ENGINEERING
70M20 Orbital mechanics
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/245584
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