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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)199825544U5242141993Tracking
KESTREL EYE IIM (KE2M)199842982U5235334892Tracking
DELLINGR (RBLE)199843021U5235034792Tracking
UBAKUSAT199843467U5232532391Tracking
CUBERRT199843546U5233333191Tracking
TEMPEST-D199843547U5238037392Tracking
RAINCUBE199843548U5232932491Tracking
HALOSAT199843549U5233432991Tracking
ENDUROSAT ONE199843551U5227426890Tracking
EQUISAT199843552U5233032491Tracking
RADSAT-G199843553U5235334692Tracking
1998-067PC199843554U5219818588Tracking
AEROCUBE 12A201843556U5248147094Tracking
AEROCUBE 12B201843557U5248247194Tracking
LEMUR-2-VU201843558U5247646694Tracking
LEMUR-2-ALEXANDER201843559U5247646694Tracking
LEMUR-2-YUASA201843560U5247746694Tracking
LEMUR-2-TOMHENDERSON201843561U5247746794Tracking
SIRIUSSAT-1199843595U5232532191Tracking
SIRIUSSAT-2199843596U5232532191Tracking
1998-067PN199843638U5237136892Tracking
1998-067PP199843639U5235234892Tracking
STARS-ME199843640U5236636192Tracking
ISS DEB (SEDA-AP)199843870U5239538992Tracking
CATSAT-2199844029U5236535992Tracking
DELPHINI199844030U5236135592Tracking
UNITE199844031U5238137692Tracking
CATSAT-1199844033U5236535992Tracking
ISS DEB199844303U5240539893Tracking
ISS DEB199844304U5237337092Tracking
ISS DEB199844305U5236135792Tracking
ISS DEB199844306U5240639793Tracking
RAAVANA-1199844329U5239238492Tracking
UGUISU199844330U5239238492Tracking
NEPALISAT-1199844331U5239238492Tracking
SPOOQY-1199844332U5239138592Tracking
RED-EYE 1 (PINOT)199844364U5240739893Tracking
IOD-1 GEMS199844385U5237837692Tracking
SWIATOWID199844426U5237437192Tracking
KRAKSAT199844427U5239739392Tracking
VCC A199844428U5239138892Tracking
ENTRYSAT199844429U5238738592Tracking
VCC C199844430U5238237992Tracking
VCC B199844431U5239138892Tracking
ISS DEB199844788U5239438892Tracking
ISS DEB199844789U5239738992Tracking
RWASAT-1199844790U5241140093Tracking
AQT-D199844791U5241040193Tracking
NARSSCUBE-1199844792U5240539893Tracking
STPSAT-4199845043U5241941193Tracking
HARP199845256U5241540693Tracking
1998-067RA199845257U5241640593Tracking
PHOENIX199845258U5241640893Tracking
1998-067RC199845259U5241440493Tracking
CRYOCUBE199845260U5241440393Tracking
AZTECHSAT-1199845261U5241240193Tracking
RADSAT-U199845262U5241640693Tracking
QARMAN199845263U5241440493Tracking
SORTIE199845264U5241840893Tracking
ICS-EF (ISS DEB)199845265U5242041293Tracking
SOYUZ-MS 16202045476U5242141993Tracking
PROGRESS-MS 14202045595U5242141993Tracking
G-SAT199845597U5241640893Tracking
QUETZAL-1199845598U5241541093Tracking
RED-EYE 2 (MERLOT)199845800U5241841593Tracking
RED-EYE 3 (CABERNET)199845809U5241841593Tracking
PROGRESS-MS 15202045937U5242141993Tracking
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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