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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)199825544U52º42041993Tracking
KESTREL EYE IIM (KE2M)199842982U52º35434992Tracking
DELLINGR (RBLE)199843021U52º35134892Tracking
UBAKUSAT199843467U52º32832591Tracking
CUBERRT199843546U52º33533291Tracking
TEMPEST-D199843547U52º38037392Tracking
RAINCUBE199843548U52º33232691Tracking
HALOSAT199843549U52º33633091Tracking
ENDUROSAT ONE199843551U52º28427890Tracking
EQUISAT199843552U52º33332691Tracking
RADSAT-G199843553U52º35534792Tracking
1998-067PC199843554U52º24323389Tracking
AEROCUBE 12A201843556U52º48147094Tracking
AEROCUBE 12B201843557U52º48247194Tracking
LEMUR-2-VU201843558U52º47646794Tracking
LEMUR-2-ALEXANDER201843559U52º47646694Tracking
LEMUR-2-YUASA201843560U52º47646794Tracking
LEMUR-2-TOMHENDERSON201843561U52º47746794Tracking
SIRIUSSAT-1199843595U52º32832391Tracking
SIRIUSSAT-2199843596U52º32832491Tracking
1998-067PN199843638U52º37236892Tracking
1998-067PP199843639U52º35434992Tracking
STARS-ME199843640U52º36736192Tracking
ISS DEB (SEDA-AP)199843870U52º39538992Tracking
CATSAT-2199844029U52º36636092Tracking
DELPHINI199844030U52º36235692Tracking
UNITE199844031U52º38237692Tracking
CATSAT-1199844033U52º36636092Tracking
ISS DEB199844303U52º40539993Tracking
ISS DEB199844304U52º37437192Tracking
ISS DEB199844305U52º36335992Tracking
ISS DEB199844306U52º40639893Tracking
RAAVANA-1199844329U52º39238592Tracking
UGUISU199844330U52º39338592Tracking
NEPALISAT-1199844331U52º39238592Tracking
SPOOQY-1199844332U52º39238692Tracking
RED-EYE 1 (PINOT)199844364U52º40739893Tracking
IOD-1 GEMS199844385U52º37937792Tracking
SWIATOWID199844426U52º37537392Tracking
KRAKSAT199844427U52º39739492Tracking
VCC A199844428U52º39238992Tracking
ENTRYSAT199844429U52º38838592Tracking
VCC C199844430U52º38338092Tracking
VCC B199844431U52º39238992Tracking
ISS DEB199844788U52º39538992Tracking
ISS DEB199844789U52º39839092Tracking
RWASAT-1199844790U52º41240093Tracking
AQT-D199844791U52º41140193Tracking
NARSSCUBE-1199844792U52º40639893Tracking
STPSAT-4199845043U52º41941193Tracking
HARP199845256U52º41640693Tracking
1998-067RA199845257U52º41740693Tracking
PHOENIX199845258U52º41640893Tracking
1998-067RC199845259U52º41440493Tracking
CRYOCUBE199845260U52º41440393Tracking
AZTECHSAT-1199845261U52º41240293Tracking
RADSAT-U199845262U52º41640693Tracking
QARMAN199845263U52º41540593Tracking
SORTIE199845264U52º41940893Tracking
ICS-EF (ISS DEB)199845265U52º42041293Tracking
SOYUZ-MS 16202045476U52º42041993Tracking
PROGRESS-MS 14202045595U52º42041993Tracking
G-SAT199845597U52º41640893Tracking
QUETZAL-1199845598U52º41541093Tracking
RED-EYE 2 (MERLOT)199845800U52º41841593Tracking
RED-EYE 3 (CABERNET)199845809U52º41841593Tracking
PROGRESS-MS 15202045937U52º42041993Tracking
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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