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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)199825544U5240940193Tracking
FLOCK 2E'-14199841762U5232632491Tracking
FLOCK 2E'-15199841764U5233233191Tracking
TIANGONG-2201641765U4339538492Tracking
FLOCK 2E'-18199841769U5233233191Tracking
FLOCK 2E'-20199841782U5230729991Tracking
BANXING-2201641834U4333632191Tracking
ITF-2199841932U5233032791Tracking
WASEDA-SAT3199841933U5229729390Tracking
AOBA-VELOX 3199841935U5231130891Tracking
LEMUR-2-REDFERN-GOES199842059U5232632391Tracking
LEMUR-2-AUSTINTACIOUS199842068U5229629390Tracking
LEMUR-2-TRUTNAHD199842069U5231831791Tracking
HAVELSAT199842700U5234734491Tracking
CXBN-2199842704U5234834691Tracking
ICECUBE199842705U5230530291Tracking
PHOENIX199842706U5235535492Tracking
X-CUBESAT199842707U5234334391Tracking
QBEE50-LTU-OC199842708U5234734691Tracking
ALTAIR PATHFINDER199842711U5237336892Tracking
SHARC199842712U5236936692Tracking
ZA-AEROSAT199842713U5236035792Tracking
LINK199842714U5230029490Tracking
CSUNSAT 1199842715U5235835492Tracking
SPACECUBE199842717U5234834691Tracking
HOOPOE199842718U5233633591Tracking
NJUST-1199842722U5236535892Tracking
UNSW-ECO199842723U5233333091Tracking
LILACSAT-1199842725U5235435092Tracking
NSIGHT-1199842726U5238437792Tracking
SNUSAT-1199842727U5235534992Tracking
I-INSPIRE II199842731U5233132791Tracking
POLYITAN-2-SAU199842732U5234634191Tracking
SNUSAT-1B199842733U5235234792Tracking
EXALTA-1199842734U5232732491Tracking
BEEAGLESAT199842736U5235835292Tracking
ASTERIA199843020U5238838492Tracking
DELLINGR (RBLE)199843021U5239439192Tracking
OSIRIS-3U199843027U5236736492Tracking
PROGRESS-MS 08201843211U5240940193Tracking
SOYUZ-MS 08201843238U5240940193Tracking
1KUNS-PF199843466U5239739692Tracking
UBAKUSAT199843467U5240039693Tracking
BATSU-CS1 (IRAZU)199843468U5239639592Tracking
SOYUZ-MS 09201843493U5240940193Tracking
PROGRESS-MS 09201843537U5240940193Tracking
CUBERRT199843546U5240639793Tracking
TEMPEST-D199843547U5240739793Tracking
1998-067NW199843548U5240739793Tracking
HALOSAT199843549U5240739793Tracking
1998-067NY199843550U5240539793Tracking
ENDUROSAT ONE199843551U5240739693Tracking
EQUISAT199843552U5240739693Tracking
1998-067PB199843553U5240739693Tracking
1998-067PC199843554U5240739693Tracking
AEROCUBE 12A201843556U5248947694Tracking
AEROCUBE 12B201843557U5248947694Tracking
LEMUR E201843558U5248847694Tracking
LEMUR F201843559U5248847694Tracking
LEMUR G201843560U5248947694Tracking
LEMUR H201843561U5248947694Tracking
SIRIUSSAT 1199843595U5240740193Tracking
1998-067PH199843596U5240840093Tracking
1998-067PJ199843597U5240940093Tracking
1998-067PK199843598U5240840193Tracking
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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