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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.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
ISS (ZARYA)199825544U52º42041293Tracking
AEROCUBE 12A201843556U52º44743993Tracking
AEROCUBE 12B201843557U52º45444594Tracking
LEMUR-2-VU201843558U52º42041393Tracking
LEMUR-2-ALEXANDER201843559U52º41640993Tracking
LEMUR-2-YUASA201843560U52º41941293Tracking
LEMUR-2-TOMHENDERSON201843561U52º42641993Tracking
ISS DEB (SEDA-AP)199843870U52º28628190Tracking
STPSAT-4199845043U52º31431091Tracking
SORTIE199845264U52º29829290Tracking
ICS-EF (ISS DEB)199845265U52º37637192Tracking
RED-EYE 2 (MERLOT)199845800U52º34334391Tracking
RED-EYE 3 (CABERNET)199845809U52º34434291Tracking
ISS DEB199847853U52º40540293Tracking
MMSATS-1199847976U52º38438392Tracking
CSS (TIANHE)202148274U41º38638192Tracking
ISS DEB199848833U52º36035892Tracking
RAMSAT199848850U52º33332891Tracking
BD-28199848867U52º30830091Tracking
ISS (NAUKA)202149044U52º42041293Tracking
FREGAT DEB201149271U52º2456979121Tracking
BINAR-1199849272U52º32732391Tracking
CUAVA-1199849275U52º28227090Tracking
CAPSAT199849276U52º31731191Tracking
PR-CUNAR 2199849277U52º28727690Tracking
1998-067TD199851441U52º36836292Tracking
PATCOOL199851442U52º36736192Tracking
LIGHT-1199851509U52º38337492Tracking
PROGRESS-MS 19202251660U52º42041293Tracking
SOYUZ-MS 21202252086U52º42041293Tracking
IHI-SAT199852147U52º38838392Tracking
KITSUNE199852148U52º39939392Tracking
CREW DRAGON 4202252318U52º42041293Tracking
TIANZHOU-4202252509U41º38638192Tracking
PROGRESS-MS 20202252795U52º42041293Tracking
SHENZHOU 14202252797U41º38638192Tracking
ISS DEB199852952U52º40840293Tracking
DRAGON CRS-25202253113U52º42041293Tracking
CSS (WENTIAN)202253239U41º38638192Tracking
1998-067TQ199853305U52º41541093Tracking
1998-067TR199853306U52º41441093Tracking
1998-067TS199853307U52º41441093Tracking
RS3S199853308U52º41441093Tracking
RS1S199853309U52º41440993Tracking
RS5S199853310U52º41441093Tracking
RS6S199853311U52º41341093Tracking
RS9S199853312U52º41440993Tracking
RS12S199853313U52º41440993Tracking
RS4S199853321U52º41441093Tracking
1998-067UA199853322U52º41441093Tracking
1998-067UB199853462U52º41940893Tracking
1998-067UC199853463U52º41940893Tracking
1998-067UD199853464U52º41940893Tracking
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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