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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)199825544U5240840193Tracking
TIANGONG-2201641765U4339138392Tracking
BANXING-2201641834U4332030391Tracking
ITF-2199841932U5226526090Tracking
HAVELSAT199842700U5231230691Tracking
CXBN-2199842704U5231330991Tracking
PHOENIX199842706U5233533291Tracking
X-CUBESAT199842707U5230129690Tracking
QBEE50-LTU-OC199842708U5231230891Tracking
ALTAIR PATHFINDER199842711U5236135692Tracking
SHARC199842712U5234634291Tracking
ZA-AEROSAT199842713U5234033691Tracking
CSUNSAT 1199842715U5233533091Tracking
SPACECUBE199842717U5231430991Tracking
HOOPOE199842718U5225024189Tracking
NJUST-1199842722U5234834091Tracking
LILACSAT-1199842725U5232632091Tracking
NSIGHT-1199842726U5237636992Tracking
SNUSAT-1199842727U5232832191Tracking
POLYITAN-2-SAU199842732U5230229791Tracking
SNUSAT-1B199842733U5232031491Tracking
BEEAGLESAT199842736U5233432791Tracking
KESTREL EYE IIM (KE2M)199842982U5239138592Tracking
ASTERIA199843020U5237837592Tracking
DELLINGR (RBLE)199843021U5239038592Tracking
OSIRIS-3U199843027U5233332891Tracking
1KUNS-PF199843466U5238938792Tracking
UBAKUSAT199843467U5239438992Tracking
BATSU-CS1 (IRAZU)199843468U5238638492Tracking
SOYUZ-MS 09201843493U5240940193Tracking
PROGRESS-MS 09201843537U5240940193Tracking
CUBERRT199843546U5239638892Tracking
TEMPEST-D199843547U5240439593Tracking
RAINCUBE199843548U5240039192Tracking
HALOSAT199843549U5240039192Tracking
1998-067NY199843550U5239538892Tracking
ENDUROSAT ONE199843551U5239938992Tracking
EQUISAT199843552U5240039092Tracking
1998-067PB199843553U5240139192Tracking
1998-067PC199843554U5239838992Tracking
AEROCUBE 12A201843556U5248847594Tracking
AEROCUBE 12B201843557U5248847594Tracking
LEMUR-2-VU201843558U5248647594Tracking
LEMUR-2-ALEXANDER201843559U5248647594Tracking
LEMUR-2-TOMHENDERSON201843560U5248647494Tracking
LEMUR-2-YUASA201843561U5248647494Tracking
SIRIUSSAT-1199843595U5240039493Tracking
SIRIUSSAT-2199843596U5240139493Tracking
TANUSHA-3199843597U5239939392Tracking
1998-067PK199843598U5240039392Tracking
1998-067PN199843638U5240439993Tracking
1998-067PP199843639U5240539693Tracking
STARS-ME199843640U5240539693Tracking
PROGRESS-MS 10201843702U5240940193Tracking
CYGNUS NG-10201843704U5240940193Tracking
SOYUZ-MS 11201843756U5240940193Tracking
DRAGON CRS-16201843827U5240940193Tracking
DRAGON CRS-16 DEB201843828U5218416388Tracking
1998-067PS199843847U5240339693Tracking
1998-067PT199843848U5237934592Tracking
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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