COMS 1

36744
Nummer im Katalog Spacetrack
2010-06-26
In die Umlaufbahn bringen
35786.35 km
Höhe Durchschnitt
11068.95 km/h
Durchschnittsgeschwindigkeit

Informationen über den Satelliten. COMS 1 - CHOLLIAN

Name im Katalog Spacetrack COMS 1
Alternative Bezeichnung CHOLLIAN
Folge COMS 1 COMS 1 Tracker
Flugzeiten COMS 1 Flugzeiten COMS 1
In die Umlaufbahn bringen 2010-06-26 (14 vor Jahren)
Tage im Orbit 5461
Herkunftsland/-organisation Korea (SKOR)
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. FRGUI (Guiana Space Centre, French Guiana)
Kategorie
Perygeum 35782 km
Apogäum 35791 km
Neigung der Umlaufbahn (Inklination) 3.85°
Runden pro Tag 1
Orbit GEO
Höhe COMS 1 35786.35 km

Informationen über COMS 1

Chollian, (Korean, lit. Thousand Li View) also known as Communication, Ocean and Meteorological Satellite 1 (COMS-1), is a South Korean satellite which was launched in June, 2010. It will be operated by the Korea Aerospace Research Institute, who will use it for communication, oceanography, and meteorological observation.
COMS-1 was constructed by EADS Astrium, and is based on the Eurostar-3000S satellite bus, bringing together ESA-made heritage from Meteosat and lessons learned from Eurostar satellites respectively. It has a mass of 2,460 kilograms (5,420 lb), and carries transponders broadcasting in the D/E and K bands of the NATO-defined spectrum, or the L/S and Ka bands of the IEEE-defined spectrum respectively. Its single solar array is expected to generate a minimum of 2.5 kilowatts of power.COMS-1 was launched by Arianespace using an Ariane 5ECA carrier rocket lifting off from ELA-3 at the Guiana Space Centre in Kourou, French Guiana. The first attempt to launch it occurred on 23 June 2010, however the launch was scrubbed due to a problem with one of the rocket's subsystems. A subsequent attempt on 24 June was also scrubbed, due to a problem with the pressurisation of the rocket's fuel tanks. The launch occurred at 21:41 UTC on 26 June 2010. The Saudi Arabian Arabsat-5A satellite was launched by the same rocket, with a SYLDA adaptor being used to separate the spacecraft. Arabsat-5A was mounted atop the SYLDA, with COMS-1 underneath it.Following launch, COMS-1 separated into a geosynchronous transfer orbit. It will use an apogee motor to raise itself into geosynchronous orbit. Once it reaches this orbit, it will undergo testing before beginning operations at a longitude of 128.2 degrees East. Its mission is scheduled to last seven years, however the satellite has a design life of ten years.


== References ==

der Satellit COMS 1 hinausgetragen 26.06.2010r. Durchschnittshöhe COMS 1 Text Nummer 1: das. 35786.35 km. Durchschnittsgeschwindigkeit COMS 1 beträgt 11068.95 km/h. Neigung COMS 1 Satelliten 3.33°.

Orbital Elemente

Zeige formatiertes JSON.

Durchschnittshöhe der Orbitalbahn. COMS 1

Durchschnittsgeschwindigkeit COMS 1

Durchschnitt COMS 1

Aktualisierungsdatum.: 2025-06-08 23:07:38
Durchschnittshöhe COMS 1 beträgt: 35786.35km
Durchschnittsgeschwindigkeit COMS 1 beträgt: 11068.95km/h
Durchschnittliche Neigung der Bahn COMS 1 beträgt: 3.33°
COMS 1 wurde am Tag in eine Umlaufbahn gebracht 2010-06-26
COMS 1 ist von 5461 Tage in der Umlaufbahn.