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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)199825544U52º42241793Tracking
KESTREL EYE IIM (KE2M)199842982U52º32531991Tracking
DELLINGR (RBLE)199843021U52º31431291Tracking
TEMPEST-D199843547U52º34133691Tracking
RADSAT-G199843553U52º29428890Tracking
AEROCUBE 12A201843556U52º47846794Tracking
AEROCUBE 12B201843557U52º48046894Tracking
LEMUR-2-VU201843558U52º47246294Tracking
LEMUR-2-ALEXANDER201843559U52º47246194Tracking
LEMUR-2-YUASA201843560U52º47346294Tracking
LEMUR-2-TOMHENDERSON201843561U52º47446394Tracking
1998-067PN199843638U52º34834691Tracking
1998-067PP199843639U52º26826290Tracking
STARS-ME199843640U52º33333091Tracking
ISS DEB (SEDA-AP)199843870U52º38838392Tracking
CATSAT-2199844029U52º31030491Tracking
DELPHINI199844030U52º27526790Tracking
UNITE199844031U52º36035692Tracking
CATSAT-1199844033U52º31130591Tracking
ISS DEB199844303U52º39839292Tracking
ISS DEB199844304U52º29328690Tracking
ISS DEB199844306U52º39839092Tracking
RAAVANA-1199844329U52º36836392Tracking
UGUISU199844330U52º36936492Tracking
NEPALISAT-1199844331U52º36836392Tracking
SPOOQY-1199844332U52º36936592Tracking
RED-EYE 1 (PINOT)199844364U52º39939192Tracking
IOD-1 GEMS199844385U52º31831391Tracking
SWIATOWID199844426U52º28727990Tracking
KRAKSAT199844427U52º38237992Tracking
VCC A199844428U52º37036892Tracking
ENTRYSAT199844429U52º35835792Tracking
VCC C199844430U52º34033791Tracking
VCC B199844431U52º36936792Tracking
ISS DEB199844788U52º35034691Tracking
ISS DEB199844789U52º35835492Tracking
RWASAT-1199844790U52º40039292Tracking
AQT-D199844791U52º40039292Tracking
NARSSCUBE-1199844792U52º38838392Tracking
STPSAT-4199845043U52º41240693Tracking
HARP199845256U52º40439693Tracking
1998-067RA199845257U52º40639793Tracking
PHOENIX199845258U52º40740093Tracking
1998-067RC199845259U52º39939192Tracking
CRYOCUBE199845260U52º39839092Tracking
AZTECHSAT-1199845261U52º39438692Tracking
RADSAT-U199845262U52º40539793Tracking
QARMAN199845263U52º40039292Tracking
SORTIE199845264U52º41240393Tracking
ICS-EF (ISS DEB)199845265U52º41640993Tracking
PROGRESS-MS 14202045595U52º42241793Tracking
G-SAT199845597U52º40539993Tracking
QUETZAL-1199845598U52º40139893Tracking
RED-EYE 2 (MERLOT)199845800U52º41141093Tracking
RED-EYE 3 (CABERNET)199845809U52º41241093Tracking
DEMI199845916U52º40340193Tracking
TECHEDSAT 10199845917U52º31630691Tracking
SOYUZ-MS 17202046613U52º42241793Tracking
CREW DRAGON 1202046920U52º42241793Tracking
SPOC199846921U52º41240993Tracking
BOBCAT-1199846922U52º40940793Tracking
NEUTRON-1199846923U52º41240993Tracking
1998-067RU199846924U52º40540393Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º40440293Tracking
LEMUR-2-DJARA199846926U52º40540293Tracking
DESCENT199846927U52º41240993Tracking
PROGRESS-MS 16202147618U52º42241793Tracking
CYGNUS NG-15202147689U52º42241793Tracking
ANTARES R/B202147690U52º21816288Tracking
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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