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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)199825544U5242041193Tracking
ALTAIR PATHFINDER199842711U5231931391Tracking
NSIGHT199842726U5235234692Tracking
KESTREL EYE IIM (KE2M)199842982U5238037592Tracking
ASTERIA199843020U5235334992Tracking
DELLINGR (RBLE)199843021U5237837592Tracking
1KUNS-PF199843466U5236536492Tracking
UBAKUSAT199843467U5237837592Tracking
BATSU-CS1 (IRAZU)199843468U5235535392Tracking
CUBERRT199843546U5237336792Tracking
TEMPEST-D199843547U5239638892Tracking
RAINCUBE199843548U5238437792Tracking
HALOSAT199843549U5238437792Tracking
RADIX199843550U5236636192Tracking
ENDUROSAT ONE199843551U5237937292Tracking
EQUISAT199843552U5238437692Tracking
1998-067PB199843553U5238837992Tracking
1998-067PC199843554U5237837092Tracking
AEROCUBE 12A201843556U5248547494Tracking
AEROCUBE 12B201843557U5248547494Tracking
LEMUR-2-VU201843558U5248247294Tracking
LEMUR-2-ALEXANDER201843559U5248247294Tracking
LEMUR-2-YUASA201843560U5248247294Tracking
LEMUR-2-TOMHENDERSON201843561U5248347294Tracking
SIRIUSSAT-1199843595U5238337992Tracking
SIRIUSSAT-2199843596U5238437992Tracking
TANUSHA-3199843597U5237937492Tracking
1998-067PK199843598U5237837392Tracking
1998-067PN199843638U5239339092Tracking
1998-067PP199843639U5239038492Tracking
STARS-ME199843640U5239338692Tracking
ISS DEB (SEDA-AP)199843870U5240339893Tracking
CATSAT-2199844029U5239939292Tracking
DELPHINI199844030U5239839292Tracking
UNITE199844031U5240139693Tracking
TECHEDSAT 8199844032U5238438092Tracking
CATSAT-1199844033U5239939292Tracking
SOYUZ-MS 12201944069U5242141093Tracking
CYGNUS NG-11201944188U5248346694Tracking
ISS DEB199844303U5241540793Tracking
ISS DEB199844304U5241240493Tracking
ISS DEB199844305U5241040393Tracking
ISS DEB199844306U5241640793Tracking
NEPALISAT-1199844329U5241440493Tracking
RAAVANA-1199844330U5241440593Tracking
UGUISU199844331U5241440493Tracking
SPOOQY-1199844332U5241340593Tracking
RED-EYE199844364U5241640793Tracking
IOD-1 GEMS199844385U5241240893Tracking
SWIATOWID199844426U5241340893Tracking
KRAKSAT199844427U5241340993Tracking
VCC A199844428U5241240893Tracking
VCC B199844429U5241240893Tracking
VCC C199844430U5241240893Tracking
ENTRYSAT199844431U5241240893Tracking
SOYUZ-MS 13201944437U5242141093Tracking
DRAGON CRS-18201944446U5242141093Tracking
DRAGON CRS-18 DEB201944447U5219016688Tracking
DRAGON CRS-18 DEB201944448U5216814488Tracking
PROGRESS-MS 12201944455U5242141193Tracking
SL-4 R/B201944456U5212811987Tracking
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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