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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)199825544U5241140493Tracking
TIANGONG-2201641765U4339238192Tracking
BANXING-2201641834U4331429791Tracking
ITF-2199841932U5215415388Tracking
HAVELSAT199842700U5228828490Tracking
CXBN-2199842704U5229028690Tracking
PHOENIX199842706U5232532491Tracking
X-CUBESAT199842707U5225825290Tracking
QBEE50-LTU-OC199842708U5228828490Tracking
ALTAIR PATHFINDER199842711U5235535392Tracking
SHARC199842712U5233433291Tracking
ZA-AEROSAT199842713U5232932991Tracking
CSUNSAT 1199842715U5232332291Tracking
SPACECUBE199842717U5229028690Tracking
NJUST-1199842722U5233933591Tracking
LILACSAT-1199842725U5230930691Tracking
NSIGHT-1199842726U5237436892Tracking
SNUSAT-1199842727U5231030991Tracking
POLYITAN-2-SAU199842732U5226025590Tracking
SNUSAT-1B199842733U5229929990Tracking
BEEAGLESAT199842736U5232131791Tracking
KESTREL EYE IIM (KE2M)199842982U5238938492Tracking
ASTERIA199843020U5237437392Tracking
DELLINGR (RBLE)199843021U5238738592Tracking
OSIRIS-3U199843027U5231030791Tracking
1KUNS-PF199843466U5238538492Tracking
UBAKUSAT199843467U5239038892Tracking
BATSU-CS1 (IRAZU)199843468U5238238192Tracking
PROGRESS-MS 09201843537U5241140493Tracking
CUBERRT199843546U5239338692Tracking
TEMPEST-D199843547U5240239593Tracking
RAINCUBE199843548U5239739092Tracking
HALOSAT199843549U5239739092Tracking
1998-067NY199843550U5239138592Tracking
ENDUROSAT ONE199843551U5239538892Tracking
EQUISAT199843552U5239738992Tracking
1998-067PB199843553U5239839092Tracking
1998-067PC199843554U5239538792Tracking
AEROCUBE 12A201843556U5248747694Tracking
AEROCUBE 12B201843557U5248747694Tracking
LEMUR-2-VU201843558U5248547594Tracking
LEMUR-2-ALEXANDER201843559U5248547594Tracking
LEMUR-2-YUASA201843560U5248547494Tracking
LEMUR-2-TOMHENDERSON201843561U5248547494Tracking
SIRIUSSAT-1199843595U5239739392Tracking
SIRIUSSAT-2199843596U5239839392Tracking
TANUSHA-3199843597U5239639292Tracking
1998-067PK199843598U5239639292Tracking
1998-067PN199843638U5240139993Tracking
1998-067PP199843639U5240239593Tracking
STARS-ME199843640U5240239693Tracking
PROGRESS-MS 10201843702U5241140493Tracking
CYGNUS NG-10201843704U5241140493Tracking
SOYUZ-MS 11201843756U5241140493Tracking
DRAGON CRS-16201843827U5240740493Tracking
ISS DEB199843847U5231527390Tracking
OBJECT PU199843870U5240740293Tracking
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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