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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)199825544U5241140393Tracking
TIANGONG-2201641765U4339038192Tracking
BANXING-2201641834U4331028991Tracking
HAVELSAT199842700U5224423489Tracking
CXBN-2199842704U5225024089Tracking
PHOENIX199842706U5231731491Tracking
X-CUBESAT199842707U5217316588Tracking
QBEE50-LTU-OC199842708U5224122989Tracking
ALTAIR PATHFINDER199842711U5235234892Tracking
SHARC199842712U5232332091Tracking
ZA-AEROSAT199842713U5232331991Tracking
CSUNSAT 1199842715U5231431091Tracking
SPACECUBE199842717U5224923989Tracking
NJUST-1199842722U5233332891Tracking
LILACSAT-1199842725U5229128690Tracking
NSIGHT-1199842726U5237236592Tracking
SNUSAT-1B199842727U5229528890Tracking
POLYITAN-2-SAU199842732U5217316488Tracking
SNUSAT-1199842733U5227726990Tracking
BEEAGLESAT199842736U5231030691Tracking
KESTREL EYE IIM (KE2M)199842982U5238838292Tracking
ASTERIA199843020U5237336992Tracking
DELLINGR (RBLE)199843021U5238638392Tracking
OSIRIS-3U199843027U5227926990Tracking
1KUNS-PF199843466U5238238292Tracking
UBAKUSAT199843467U5238938692Tracking
BATSU-CS1 (IRAZU)199843468U5237837892Tracking
CUBERRT199843546U5239038392Tracking
TEMPEST-D199843547U5240239393Tracking
RAINCUBE199843548U5239638892Tracking
HALOSAT199843549U5239638892Tracking
1998-067NY199843550U5238838292Tracking
ENDUROSAT ONE199843551U5239338592Tracking
EQUISAT199843552U5239538792Tracking
1998-067PB199843553U5239738892Tracking
1998-067PC199843554U5239338592Tracking
AEROCUBE 12A201843556U5248747594Tracking
AEROCUBE 12B201843557U5248747594Tracking
LEMUR-2-VU201843558U5248547494Tracking
LEMUR-2-ALEXANDER201843559U5248547494Tracking
LEMUR-2-YUASA201843560U5248547494Tracking
LEMUR-2-TOMHENDERSON201843561U5248547494Tracking
SIRIUSSAT-1199843595U5239539192Tracking
SIRIUSSAT-2199843596U5239639192Tracking
TANUSHA-3199843597U5239438992Tracking
1998-067PK199843598U5239438992Tracking
1998-067PN199843638U5240139793Tracking
1998-067PP199843639U5240039392Tracking
STARS-ME199843640U5240239493Tracking
PROGRESS-MS 10201843702U5241140393Tracking
CYGNUS NG-10201843704U5231630291Tracking
SOYUZ-MS 11201843756U5241140393Tracking
ISS DEB (SEDA-AP)199843870U5240740093Tracking
CATSAT-1199844029U5240840193Tracking
DELPHINI199844030U5240840193Tracking
UNITE199844031U5240740293Tracking
TECHEDSAT 8199844032U5240640193Tracking
CATSAT-2199844033U5240840193Tracking
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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