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International Space Station Stuff
In this category are all related satellite for International Space Station, including the Soyuz spacecraft, Progress spacecraft, Dragon module, Tiangong or ATV modules.
Satellite Launch Norad Incl.
ISS (ZARYA)199825544U5242241493Tracking
ISS DEB199847853U5234634491Tracking
CSS (TIANHE)202148274U4138537492Tracking
ISS (NAUKA)202149044U5242241493Tracking
FREGAT DEB201149271U522401907119Tracking
CSS (WENTIAN)202253239U4138537492Tracking
CSS (MENGTIAN)202254216U4138537492Tracking
ISS DEB (SPX-26 IPA FSE)199855448U5235934892Tracking
SOYUZ-MS 23202355688U5242241493Tracking
ARKSAT 1199856311U5234533491Tracking
ISS DEB199856434U5237636592Tracking
PROGRESS-MS 23202356740U5242241493Tracking
SHENZHOU-16 (SZ-16)202356761U4138537492Tracking
ISS DEB199857212U5240539793Tracking
CYGNUS NG-19202357488U5242241493Tracking
PROGRESS-MS 24202357691U5242241493Tracking
CREW DRAGON 7202357697U5242241493Tracking
SOYUZ-MS 24202357862U5242241493Tracking
Satellites Orbital Parameters

The table above shows the main parameters and information available for this satellite.

Satellite: This column shows the name of the object in orbit. In some cases the official name ends with the words R/B, meaning that it is a piece or any stage from some rocket booster.

Norad: North American Aerospace Defense Command, the Air Defence Command of the United States, responsible for the catalogue of objects in orbit. The number indicates the record of the satellite in the Norad archives.

Inclination: Angle formed between the orbit of the satellite and terrestrial line of the equator. Satellites with inclination of 0 degrees follow the equator line and are called equatorial orbit satellites. When the inclination is 90 degrees its orbit crosses the terrestrial poles and are called polar orbiting satellites. When the inclination is less or equal latitude of the place of observation, the satellite be seen directly if conditions permit.

Apogee: Maximum distance that the object is far from the center of the Earth.

Perigee: Highest approchement between the object and the center of the Earth. The figures shown already discounting the radius of the Earth, 6378 Km. One Perigee value equal to the value of Apogee indicates a circular orbit satellite.

Period: Value in minutes that a satellite takes to complete one orbit of perigee to perigee. Satellites in polar orbit, positioned at 800 km in altitude will take approximately 102 minutes to complete one revolution. The International Space Station, 350 km above the surface, completes its orbit in 90 minutes.

The lower the altitude of a satellite, more speed he needs to keep in orbit and not re-enters the atmosphere.

Geostationary satellites have a period of approximately 1436 minutes with inclination of 0 degrees (equatorial orbit). Because this is the same time it takes Earth to complete one turn on its axis, geostationary satellites appear static on the same geographic point. To this happens the satellite should be positioned about 36 thousand kilometers in altitude.

Note and Frequency: Filled with additional information where possible. The frequencies shown, when provided, are those captured by enthusiasts or informed by the official organizations of disclosure.

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