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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)199825544U5242141593Tracking
SIMPL199842983U5230229691Tracking
AEROCUBE 12A201843556U5245644794Tracking
AEROCUBE 12B201843557U5246145294Tracking
LEMUR-2-VU201843558U5243742793Tracking
LEMUR-2-ALEXANDER201843559U5243542693Tracking
LEMUR-2-YUASA201843560U5243642793Tracking
LEMUR-2-TOMHENDERSON201843561U5244043293Tracking
ISS DEB (SEDA-AP)199843870U5233432791Tracking
ISS DEB199844303U5231530991Tracking
ISS DEB199844306U5228828290Tracking
RED-EYE 1 (PINOT)199844364U5232431591Tracking
STPSAT-4199845043U5235935092Tracking
PHOENIX199845258U5229829090Tracking
SORTIE199845264U5235334492Tracking
ICS-EF (ISS DEB)199845265U5238938192Tracking
RED-EYE 2 (MERLOT)199845800U5237136592Tracking
RED-EYE 3 (CABERNET)199845809U5237136592Tracking
SPOC199846921U5231831291Tracking
NEUTRON-1199846923U5231531091Tracking
DESCENT199846927U5230530091Tracking
ISS DEB199847853U5240840693Tracking
RSP-01199847925U5230029490Tracking
TSURU199847927U5233432791Tracking
MAYA-2199847929U5233232591Tracking
GUARANISAT-1199847931U5232932391Tracking
MMSATS-1199847976U5239539492Tracking
TIANHE202148274U4139038692Tracking
ISS DEB199848833U5238338192Tracking
RAMSAT199848850U5237036692Tracking
BD-28199848867U5236435892Tracking
ISS (NAUKA)202149044U5242141593Tracking
TIANZHOU-3202149222U4139138692Tracking
FREGAT DEB201149271U5224431028121Tracking
BINAR-1199849272U5237236892Tracking
MAYA-3199849273U5235735292Tracking
MAYA-4199849274U5235635192Tracking
CUAVA-1199849275U5236335992Tracking
CAPSAT199849276U5237136892Tracking
PR-CUNAR 2199849277U5236536192Tracking
PROGRESS-MS 18202149379U5242141593Tracking
GASPACS199851439U5228927990Tracking
1998-067TD199851441U5239638492Tracking
PATCOOL199851442U5239538492Tracking
DAILI199851443U5234933591Tracking
LIGHT-1199851509U5240339092Tracking
GT-1199851510U5234633291Tracking
PROGRESS-MS 19202251660U5242141593Tracking
CYGNUS NG-17202251712U5242141593Tracking
SOYUZ-MS 21202252086U5242141593Tracking
IHI-SAT199852147U5240640193Tracking
KITSUNE199852148U5241040593Tracking
CREW DRAGON 4202252318U5242141593Tracking
ISS DEB199852329U5240138992Tracking
ISS DEB199852432U5238937592Tracking
TIANZHOU-4202252509U4139138692Tracking
2022-050B202252510U4130925290Tracking
2022-050C202252511U4128416689Tracking
CZ-7 R/B202252512U4126518989Tracking
CST-100 STARLINER OFT-2202252715U5237336192Tracking
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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