Optical Orbit Determination of a Geosynchronous Earth Orbit Satellite Effected by Baseline Distances between Various Ground-based Tracking Stations II: COMS Case with Analysis of Actual Observation Data

• Published in: Journal of astronomy and space sciences Vol. 32; no. 3; pp. 229 - 235
• Main Authors: Son, Ju Young, Jo, Jung Hyun, Choi, Jin, Kim, Bang-Yeop, Yoon, Joh-Na, Yim, Hong-Suh, Choi, Young-Jun, Park, Sun-Youp, Bae, Young Ho, Roh, Dong-Goo, Park, Jang-Hyun, Kim, Ji-Hye
• Format: Journal Article
• Language: Korean
• Published: 2015
• Subjects: actual observation data; simulation; satellite optical observation; satellite orbit estimation
• ISSN: 2093-5587; 2093-1409

We estimated the orbit of the Communication, Ocean and Meteorological Satellite (COMS), a Geostationary Earth Orbit (GEO) satellite, through data from actual optical observations using telescopes at the Sobaeksan Optical Astronomy Observatory (SOAO) of the Korea Astronomy and Space Science Institute (KASI), Optical Wide field Patrol (OWL) at KASI, and the Chungbuk National University Observatory (CNUO) from August 1, 2014, to January 13, 2015. The astrometric data of the satellite were extracted from the World Coordinate System (WCS) in the obtained images, and geometrically distorted errors were corrected. To handle the optically observed data, corrections were made for the observation time, light-travel time delay, shutter speed delay, and aberration. For final product, the sequential filter within the Orbit Determination Tool Kit (ODTK) was used for orbit estimation based on the results of optical observation. In addition, a comparative analysis was conducted between the precise orbit from the ephemeris of the COMS maintained by the satellite operator and the results of orbit estimation using optical observation. The orbits estimated in simulation agree with those estimated with actual optical observation data. The error in the results using optical observation data decreased with increasing number of observatories. Our results are useful for optimizing observation data for orbit estimation.