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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)199825544U5240840393Tracking
FLOCK 2E'-14199841762U5223622289Tracking
FLOCK 2E'-15199841764U5228727590Tracking
TIANGONG-2201641765U4339238492Tracking
FLOCK 2E'-18199841769U5228727490Tracking
BANXING-2201641834U4332831291Tracking
ITF-2199841932U5230930191Tracking
AOBA-VELOX 3199841935U5225123889Tracking
LEMUR-2-REDFERN-GOES199842059U5229728890Tracking
LEMUR-2-TRUTNAHD199842069U5227826890Tracking
HAVELSAT199842700U5233232691Tracking
CXBN-2199842704U5233332891Tracking
PHOENIX199842706U5234534291Tracking
X-CUBESAT199842707U5232632291Tracking
QBEE50-LTU-OC199842708U5233232991Tracking
ALTAIR PATHFINDER199842711U5236636292Tracking
SHARC199842712U5235835492Tracking
ZA-AEROSAT199842713U5235034692Tracking
CSUNSAT 1199842715U5234734291Tracking
SPACECUBE199842717U5233332891Tracking
HOOPOE199842718U5231230691Tracking
NJUST-1199842722U5235634992Tracking
UNSW-ECO199842723U5230329490Tracking
LILACSAT-1199842725U5234133691Tracking
NSIGHT-1199842726U5237937392Tracking
SNUSAT-1199842727U5234333591Tracking
I-INSPIRE II199842731U5229728790Tracking
POLYITAN-2-SAU199842732U5232932191Tracking
SNUSAT-1B199842733U5233833191Tracking
EXALTA-1199842734U5228627490Tracking
BEEAGLESAT199842736U5234633991Tracking
ASTERIA199843020U5238338092Tracking
DELLINGR (RBLE)199843021U5239138892Tracking
OSIRIS-3U199843027U5235234792Tracking
1KUNS-PF199843466U5239239292Tracking
UBAKUSAT199843467U5239639392Tracking
BATSU-CS1 (IRAZU)199843468U5239139092Tracking
SOYUZ-MS 09201843493U5240840393Tracking
PROGRESS-MS 09201843537U5240840393Tracking
CUBERRT199843546U5240139493Tracking
TEMPEST-D199843547U5240439793Tracking
RAINCUBE199843548U5240239593Tracking
HALOSAT199843549U5240239593Tracking
1998-067NY199843550U5239939392Tracking
ENDUROSAT ONE199843551U5240139393Tracking
EQUISAT199843552U5240239493Tracking
1998-067PB199843553U5240339493Tracking
1998-067PC199843554U5240139393Tracking
AEROCUBE 12A201843556U5248747694Tracking
AEROCUBE 12B201843557U5248847794Tracking
LEMUR-2-VU201843558U5248647694Tracking
LEMUR-2-ALEXANDER201843559U5248647694Tracking
LEMUR-2-TOMHENDERSON201843560U5248747694Tracking
LEMUR-2-YUASA201843561U5248747694Tracking
SIRIUSSAT-1199843595U5240239893Tracking
SIRIUSSAT-2199843596U5240339893Tracking
TANUSHA-3199843597U5240239893Tracking
1998-067PK199843598U5240239893Tracking
HTV-7 (KOUNOTORI 7)201843630U5240840393Tracking
1998-067PN199843638U5240540293Tracking
1998-067PP199843639U5240640093Tracking
STARS-ME199843640U5240639993Tracking
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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