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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)199825544U52º42041893Tracking
KESTREL EYE IIM (KE2M)199842982U52º34133891Tracking
DELLINGR (RBLE)199843021U52º33733591Tracking
UBAKUSAT199843467U52º27927290Tracking
TEMPEST-D199843547U52º36736292Tracking
RAINCUBE199843548U52º27827190Tracking
HALOSAT199843549U52º29528990Tracking
EQUISAT199843552U52º28127490Tracking
RADSAT-G199843553U52º33433091Tracking
AEROCUBE 12A201843556U52º48046994Tracking
AEROCUBE 12B201843557U52º48147094Tracking
LEMUR-2-VU201843558U52º47446594Tracking
LEMUR-2-ALEXANDER201843559U52º47446494Tracking
LEMUR-2-YUASA201843560U52º47446594Tracking
LEMUR-2-TOMHENDERSON201843561U52º47546594Tracking
SIRIUSSAT-1199843595U52º25122689Tracking
SIRIUSSAT-2199843596U52º23822889Tracking
1998-067PN199843638U52º36136092Tracking
1998-067PP199843639U52º33132791Tracking
STARS-ME199843640U52º35335092Tracking
ISS DEB (SEDA-AP)199843870U52º39138792Tracking
CATSAT-2199844029U52º34534491Tracking
DELPHINI199844030U52º33733691Tracking
UNITE199844031U52º37136992Tracking
CATSAT-1199844033U52º34534491Tracking
ISS DEB199844303U52º40239593Tracking
ISS DEB199844304U52º35434692Tracking
ISS DEB199844305U52º32631991Tracking
ISS DEB199844306U52º40239493Tracking
RAAVANA-1199844329U52º38237692Tracking
UGUISU199844330U52º38237692Tracking
NEPALISAT-1199844331U52º38237692Tracking
SPOOQY-1199844332U52º38237792Tracking
RED-EYE 1 (PINOT)199844364U52º40339593Tracking
IOD-1 GEMS199844385U52º36235692Tracking
SWIATOWID199844426U52º35434792Tracking
KRAKSAT199844427U52º39138792Tracking
VCC A199844428U52º38338092Tracking
ENTRYSAT199844429U52º37737392Tracking
VCC C199844430U52º36836492Tracking
VCC B199844431U52º38337992Tracking
ISS DEB199844788U52º37937392Tracking
ISS DEB199844789U52º38337692Tracking
RWASAT-1199844790U52º40739693Tracking
AQT-D199844791U52º40539793Tracking
NARSSCUBE-1199844792U52º39739292Tracking
STPSAT-4199845043U52º41540993Tracking
HARP199845256U52º41040193Tracking
1998-067RA199845257U52º41140293Tracking
PHOENIX199845258U52º41240593Tracking
1998-067RC199845259U52º40739993Tracking
CRYOCUBE199845260U52º40739993Tracking
AZTECHSAT-1199845261U52º40439593Tracking
RADSAT-U199845262U52º41040393Tracking
QARMAN199845263U52º40840093Tracking
SORTIE199845264U52º41540693Tracking
ICS-EF (ISS DEB)199845265U52º41841193Tracking
PROGRESS-MS 14202045595U52º42041893Tracking
G-SAT199845597U52º41040593Tracking
QUETZAL-1199845598U52º40840693Tracking
RED-EYE 2 (MERLOT)199845800U52º41441393Tracking
RED-EYE 3 (CABERNET)199845809U52º41441393Tracking
DEMI199845916U52º41040793Tracking
TECHEDSAT 10199845917U52º38637992Tracking
PROGRESS-MS 15202045937U52º42041893Tracking
CYGNUS NG-14202046530U52º42041893Tracking
SOYUZ-MS 17202046613U52º42041893Tracking
CREW DRAGON 1202046920U52º42041893Tracking
SPOC199846921U52º41641293Tracking
BOBCAT-1199846922U52º41641293Tracking
NEUTRON-1199846923U52º41741393Tracking
1998-067RU199846924U52º41541193Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º41441093Tracking
LEMUR-2-DJARA199846926U52º41541193Tracking
DESCENT199846927U52º41741393Tracking
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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