Empirical model of motion of space debris in the geostationary region
- Authors: Bakhtigaraev N.S.1, Levkina P.A.1, Chazov V.V.2
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Affiliations:
- Institute of Astronomy
- Sternberg Astronomical Institute
- Issue: Vol 50, No 2 (2016)
- Pages: 130-135
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/170417
- DOI: https://doi.org/10.1134/S0038094616020027
- ID: 170417
Cite item
Abstract
Regular optical observations of small-sized space debris on a geosynchronous orbit are carried out at the Terskol Peak Observatory (Kabardino-Balkaria). The aim of these observations is to gather data on technogenic pollution of near-Earth space; discover small-sized space debris, determine their parameters, and catalogue them; and maintain an updated catalogue of orbits. The results obtained by processing topocentric measurements of positions of one such object are presented. This object is distinctive in that it is a small-sized fragment of the Fengyun 2D satellite (international designator 2006-053A) and moves about a Lagrangian point at 75° E with a small amplitude. The observational material was accumulated in 12 twoweek sessions within a 6-year interval from 2009 to 2014. The variability of the ratio of the maximum cross section area to the object mass is revealed, and a model of variations of this parameter is proposed. The basic period of variations is 392 days. The validity of the model was verified in a series of independent observations in March, 2015.
About the authors
N. S. Bakhtigaraev
Institute of Astronomy
Author for correspondence.
Email: nail@inasan.ru
Russian Federation, ul. Pyatnitskaya 48, Moscow, 119017
P. A. Levkina
Institute of Astronomy
Email: nail@inasan.ru
Russian Federation, ul. Pyatnitskaya 48, Moscow, 119017
V. V. Chazov
Sternberg Astronomical Institute
Email: nail@inasan.ru
Russian Federation, Universitetskii pr. 13, Moscow, 119991
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