Investigation of the influence of heliogeoactivity on the dynamics of orbital parameters of artificial satellites of the Earth

1Koval'chuk, MM, 1Hirnyak, MB, 1Baran, OA, 1Stodilka, MI, 1Vovchyk, YB, 1Bilinsky, AI, 1Blahodyr, YT, 1Virun, NV, 2Apunevych, SV
1Astronomical Observatory of Ivan Franko National University of Lviv, Lviv, Ukraine
2Ivan Franko National University of Lviv, Lviv, Ukraine
Kinemat. fiz. nebesnyh tel (Online) 2017, 33(5):68-74
https://doi.org/10.15407/kfnt2017.05.098
Start Page: Dynamics and Physics of Solar System Bodies
Language: Ukrainian
Abstract: 

The main factor of changes of behavior of artificial satellites of the Earth on the orbit is the influence of aggregate of active processes on the Sun (so-called space weather) and their response in the near-Earth environment. The influence of heliogeoactivity on the dynamics of artificial satellites was investigated. The selected objects are the uncontrolled satellites, their elements of orbits are from the database of Ukrainian network of optical stations (УМОС). As a result a comprehensive research was established relationship between the characteristics of solar activity, their response in the near-Earth environment and variations of periods P of the orbital motion of artifical satellites. These variations mainly denote changes in the density of Earth's atmosphere caused by a solar (index F10.7) and geomagnetic activity ( ΣKpindex). The correlation coefficients of P and F10.7(–0.77...–0.91) and of P and ΣKp (–0.67...–0.89) are the evidence of significant connection between them. The obtained results are good indicator of influence of helio- and geoactivity on the periods of the satellites.

Keywords: artificial satellites of the Earth, heliogeoactivity, space weather, violation of the orbital movement
References: 

1.Ts. N. Gogosheva, N. N. Klimov, and K. B. Serafimov, “Restructuring of the neutral atmosphere at altitudes of the region F of the ionosphere during geomagnetic disturbances,” Issled. Geomagn., Aeron. Fiz. Solntsa, No. 41, 7–17 (1977).

2. GOST (State Standard) 25645.115-84. Upper Atmosphere of Earth. Density Model for Ballistic Flight Support of Artificial Earth Satellites. Introduction (Izd. Standartov, Moscow, 1984).

3.V. P. Epishev, I. I. Isak, V. I. Kudak, I. I. Motrunich, I. F. Naibauer, N. I. Koshkin, A. I. Bilinskii, K. P. Martynyuk-Lototskii, Ya. T. Blagodyr, V. V. Lopachenko, V. V. Rykhal’skii, S. V. Ryshchenko, and A. V. Zhukovetskii, “Some results of studies of the behaviour of a satellite in orbit in contingency mode under the near-Earth space influence,” Kosm. Nauka Tekhnol. 18 (1), 60–67 (2012).
https://doi.org/10.15407/knit2012.01.060

4.A. I. Maslova and A. V. Pirozhenko, “Atmosphere density changes caused by the motion of spacecrafts in low Earth orbits,” Kosm. Nauka Tekhnol. 15 (1), 13–18 (2009).
https://doi.org/10.15407/knit2009.01.013

5.F. A. Santora, “Influence of the aerodynamic resistance on the motion of satellites on close-to-circular orbits in a nonspherical and changing throughout the day atmosphere,” Raketnaya Tekh. Kosmonavt. 14 (9), 53–58 (1976).
https://doi.org/10.2514/3.61454

6.E. K. Fedorov, Global Studies of the Atmosphere and Weather Forecasting (Akad. Nauk. SSSR, Moscow, 1971) [in Russian].

7.L. Guglya, M. Ryabov, S. Panishko, and A. Suharev, “Dynamic characteristics of the main indexes of the space weather and their application to the analysis monitoring observations flux densities of power radio sources on RT URAN-4,” Odessa Astron. Publ. 25, 207–209 (2012).

8.V. H. Komendant, N. I. Koshkin, M. I. Ryabov, and A. L. Sukharev, “Influence of space weather effects on the upper atmosphere according to the drag of artificial Earth satellites,” Odessa Astron. Publ. 27, 89–90 (2014).