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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)199825544U52º42141593Tracking
SIMPL199842983U52º30229691Tracking
AEROCUBE 12A201843556U52º45644794Tracking
AEROCUBE 12B201843557U52º46145294Tracking
LEMUR-2-VU201843558U52º43742793Tracking
LEMUR-2-ALEXANDER201843559U52º43542693Tracking
LEMUR-2-YUASA201843560U52º43642793Tracking
LEMUR-2-TOMHENDERSON201843561U52º44043293Tracking
ISS DEB (SEDA-AP)199843870U52º33432791Tracking
ISS DEB199844303U52º31530991Tracking
ISS DEB199844306U52º28828290Tracking
RED-EYE 1 (PINOT)199844364U52º32431591Tracking
STPSAT-4199845043U52º35935092Tracking
PHOENIX199845258U52º29829090Tracking
SORTIE199845264U52º35334492Tracking
ICS-EF (ISS DEB)199845265U52º38938192Tracking
RED-EYE 2 (MERLOT)199845800U52º37136592Tracking
RED-EYE 3 (CABERNET)199845809U52º37136592Tracking
SPOC199846921U52º31831291Tracking
NEUTRON-1199846923U52º31531091Tracking
DESCENT199846927U52º30530091Tracking
ISS DEB199847853U52º40840693Tracking
RSP-01199847925U52º30029490Tracking
TSURU199847927U52º33432791Tracking
MAYA-2199847929U52º33232591Tracking
GUARANISAT-1199847931U52º32932391Tracking
MMSATS-1199847976U52º39539492Tracking
TIANHE202148274U41º39038692Tracking
ISS DEB199848833U52º38338192Tracking
RAMSAT199848850U52º37036692Tracking
BD-28199848867U52º36435892Tracking
ISS (NAUKA)202149044U52º42141593Tracking
TIANZHOU-3202149222U41º39138692Tracking
FREGAT DEB201149271U52º24431028121Tracking
BINAR-1199849272U52º37236892Tracking
MAYA-3199849273U52º35735292Tracking
MAYA-4199849274U52º35635192Tracking
CUAVA-1199849275U52º36335992Tracking
CAPSAT199849276U52º37136892Tracking
PR-CUNAR 2199849277U52º36536192Tracking
PROGRESS-MS 18202149379U52º42141593Tracking
GASPACS199851439U52º28927990Tracking
1998-067TD199851441U52º39638492Tracking
PATCOOL199851442U52º39538492Tracking
DAILI199851443U52º34933591Tracking
LIGHT-1199851509U52º40339092Tracking
GT-1199851510U52º34633291Tracking
PROGRESS-MS 19202251660U52º42141593Tracking
CYGNUS NG-17202251712U52º42141593Tracking
SOYUZ-MS 21202252086U52º42141593Tracking
IHI-SAT199852147U52º40640193Tracking
KITSUNE199852148U52º41040593Tracking
CREW DRAGON 4202252318U52º42141593Tracking
ISS DEB199852329U52º40138992Tracking
ISS DEB199852432U52º38937592Tracking
TIANZHOU-4202252509U41º39138692Tracking
2022-050B202252510U41º30925290Tracking
2022-050C202252511U41º28416689Tracking
CZ-7 R/B202252512U41º26518989Tracking
CST-100 STARLINER OFT-2202252715U52º37336192Tracking
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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