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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)199825544U5242141493Tracking
SIMPL199842983U5226926490Tracking
AEROCUBE 12A201843556U5245344294Tracking
AEROCUBE 12B201843557U5245944794Tracking
LEMUR-2-VU201843558U5243141993Tracking
LEMUR-2-ALEXANDER201843559U5242941693Tracking
LEMUR-2-YUASA201843560U5243141893Tracking
LEMUR-2-TOMHENDERSON201843561U5243642493Tracking
ISS DEB (SEDA-AP)199843870U5231730991Tracking
ISS DEB199844303U5226725790Tracking
RED-EYE 1 (PINOT)199844364U5228527690Tracking
STPSAT-4199845043U5234133591Tracking
SORTIE199845264U5233232691Tracking
ICS-EF (ISS DEB)199845265U5238237792Tracking
RED-EYE 2 (MERLOT)199845800U5235935492Tracking
RED-EYE 3 (CABERNET)199845809U5235935492Tracking
SPOC199846921U5218417288Tracking
NEUTRON-1199846923U5215114587Tracking
ISS DEB199847853U5240740493Tracking
TSURU199847927U5225924290Tracking
MAYA-2199847929U5226424890Tracking
GUARANISAT-1199847931U5225924290Tracking
MMSATS-1199847976U5239038992Tracking
TIANHE202148274U4138838492Tracking
ISS DEB199848833U5237337092Tracking
RAMSAT199848850U5235535192Tracking
BD-28199848867U5234333891Tracking
ISS (NAUKA)202149044U5242141493Tracking
TIANZHOU-3202149222U4138838492Tracking
FREGAT DEB201149271U5223401135121Tracking
BINAR-1199849272U5235834892Tracking
MAYA-3199849273U5232531191Tracking
MAYA-4199849274U5232831591Tracking
CUAVA-1199849275U5234333291Tracking
CAPSAT199849276U5235534592Tracking
PR-CUNAR 2199849277U5234533391Tracking
1998-067TD199851441U5238537492Tracking
PATCOOL199851442U5238437392Tracking
DAILI199851443U5215915088Tracking
LIGHT-1199851509U5239438292Tracking
PROGRESS-MS 19202251660U5242141493Tracking
CYGNUS NG-17202251712U5242141493Tracking
SOYUZ-MS 21202252086U5242141493Tracking
IHI-SAT199852147U5239939292Tracking
KITSUNE199852148U5240539993Tracking
CREW DRAGON 4202252318U5242141493Tracking
ISS DEB199852329U5234832391Tracking
TIANZHOU-4202252509U4138838492Tracking
PROGRESS-MS 20202252795U5242141493Tracking
SHENZHOU 14202252797U4138838492Tracking
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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