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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)199825544U52º42141993Tracking
KESTREL EYE IIM (KE2M)199842982U52º24723589Tracking
AEROCUBE 12A201843556U52º47546494Tracking
AEROCUBE 12B201843557U52º47746694Tracking
LEMUR-2-VU201843558U52º46745894Tracking
LEMUR-2-ALEXANDER201843559U52º46745794Tracking
LEMUR-2-YUASA201843560U52º46845894Tracking
LEMUR-2-TOMHENDERSON201843561U52º46945994Tracking
1998-067PN199843638U52º29929590Tracking
ISS DEB (SEDA-AP)199843870U52º38137692Tracking
UNITE199844031U52º32131991Tracking
ISS DEB199844303U52º39038392Tracking
ISS DEB199844306U52º38938092Tracking
RAAVANA-1199844329U52º32031891Tracking
UGUISU199844330U52º32332191Tracking
NEPALISAT-1199844331U52º32131991Tracking
SPOOQY-1199844332U52º32532391Tracking
RED-EYE 1 (PINOT)199844364U52º39138392Tracking
KRAKSAT199844427U52º36235792Tracking
VCC A199844428U52º33032991Tracking
ENTRYSAT199844429U52º25624389Tracking
VCC B199844431U52º32732691Tracking
RWASAT-1199844790U52º39037992Tracking
AQT-D199844791U52º38838092Tracking
NARSSCUBE-1199844792U52º36335892Tracking
STPSAT-4199845043U52º40639993Tracking
HARP199845256U52º39138292Tracking
1998-067RA199845257U52º39538692Tracking
PHOENIX199845258U52º39939192Tracking
1998-067RC199845259U52º38037392Tracking
CRYOCUBE199845260U52º36936292Tracking
AZTECHSAT-1199845261U52º36735992Tracking
RADSAT-U199845262U52º39338592Tracking
QARMAN199845263U52º38137392Tracking
SORTIE199845264U52º40539593Tracking
ICS-EF (ISS DEB)199845265U52º41240493Tracking
G-SAT199845597U52º39338792Tracking
QUETZAL-1199845598U52º38538292Tracking
RED-EYE 2 (MERLOT)199845800U52º40640493Tracking
RED-EYE 3 (CABERNET)199845809U52º40640493Tracking
DEMI199845916U52º38938592Tracking
SPOC199846921U52º40240093Tracking
BOBCAT-1199846922U52º39639492Tracking
NEUTRON-1199846923U52º40240193Tracking
1998-067RU199846924U52º38138092Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º37737792Tracking
LEMUR-2-DJARA199846926U52º38138192Tracking
DESCENT199846927U52º40240193Tracking
ISS DEB199847853U52º41941693Tracking
RSP-01199847925U52º41140893Tracking
TAUSAT-1199847926U52º40940593Tracking
TSURU199847927U52º41140993Tracking
STARS-EC199847928U52º41140593Tracking
MMSATS-1199847976U52º41741593Tracking
SOYUZ-MS 18202148159U52º42141993Tracking
CREW DRAGON 2202148209U52º42141993Tracking
TIANHE202148274U41º38637392Tracking
TIANZHOU-2202148803U41º38637392Tracking
RAMSAT199848850U52º41841393Tracking
SOAR199848851U52º41541193Tracking
SHENZHOU-12202148852U41º38637392Tracking
BD-28199848867U52º41741493Tracking
MIR-SAT 1199848868U52º41641493Tracking
PROGRESS-MS 17202148869U52º42141993Tracking
ISS (NAUKA)202149044U52º42141993Tracking
SL-25 R/B202149045U52º23716989Tracking
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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