Empirical model of motion of space debris in the geostationary region


Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

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.

Авторлар туралы

N. Bakhtigaraev

Institute of Astronomy

Хат алмасуға жауапты Автор.
Email: nail@inasan.ru
Ресей, ul. Pyatnitskaya 48, Moscow, 119017

P. Levkina

Institute of Astronomy

Email: nail@inasan.ru
Ресей, ul. Pyatnitskaya 48, Moscow, 119017

V. Chazov

Sternberg Astronomical Institute

Email: nail@inasan.ru
Ресей, Universitetskii pr. 13, Moscow, 119991

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