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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)199825544U52º42441993Tracking
KESTREL EYE IIM (KE2M)199842982U52º14814387Tracking
AEROCUBE 12A201843556U52º47446394Tracking
AEROCUBE 12B201843557U52º47646594Tracking
LEMUR-2-VU201843558U52º46645694Tracking
LEMUR-2-ALEXANDER201843559U52º46545694Tracking
LEMUR-2-YUASA201843560U52º46645694Tracking
LEMUR-2-TOMHENDERSON201843561U52º46845794Tracking
1998-067PN199843638U52º23122089Tracking
ISS DEB (SEDA-AP)199843870U52º37837492Tracking
UNITE199844031U52º29529290Tracking
ISS DEB199844303U52º38638192Tracking
ISS DEB199844306U52º38437892Tracking
RAAVANA-1199844329U52º27827290Tracking
UGUISU199844330U52º28628190Tracking
NEPALISAT-1199844331U52º28027490Tracking
SPOOQY-1199844332U52º29228890Tracking
RED-EYE 1 (PINOT)199844364U52º38738192Tracking
KRAKSAT199844427U52º35134892Tracking
VCC A199844428U52º30329991Tracking
VCC B199844431U52º29729290Tracking
RWASAT-1199844790U52º38337792Tracking
AQT-D199844791U52º38237692Tracking
NARSSCUBE-1199844792U52º34834791Tracking
STPSAT-4199845043U52º40239793Tracking
HARP199845256U52º38437992Tracking
1998-067RA199845257U52º38938392Tracking
PHOENIX199845258U52º39438992Tracking
1998-067RC199845259U52º37036692Tracking
CRYOCUBE199845260U52º35034892Tracking
AZTECHSAT-1199845261U52º35034892Tracking
RADSAT-U199845262U52º38738292Tracking
QARMAN199845263U52º37036692Tracking
SORTIE199845264U52º40139493Tracking
ICS-EF (ISS DEB)199845265U52º41040493Tracking
G-SAT199845597U52º38738392Tracking
QUETZAL-1199845598U52º37837592Tracking
RED-EYE 2 (MERLOT)199845800U52º40340393Tracking
RED-EYE 3 (CABERNET)199845809U52º40340393Tracking
DEMI199845916U52º38237992Tracking
SPOC199846921U52º40039693Tracking
BOBCAT-1199846922U52º39238892Tracking
NEUTRON-1199846923U52º40039693Tracking
1998-067RU199846924U52º37236792Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º36736292Tracking
LEMUR-2-DJARA199846926U52º37336992Tracking
DESCENT199846927U52º40039693Tracking
ISS DEB199847853U52º41941593Tracking
RSP-01199847925U52º40840493Tracking
TAUSAT-1199847926U52º40540093Tracking
TSURU199847927U52º40940593Tracking
STARS-EC199847928U52º40839993Tracking
MMSATS-1199847976U52º41741393Tracking
SOYUZ-MS 18202148159U52º42441993Tracking
CREW DRAGON 2202148209U52º42441993Tracking
TIANHE202148274U41º38638092Tracking
TIANZHOU-2202148803U41º38638192Tracking
RAMSAT199848850U52º41741093Tracking
SOAR199848851U52º40840193Tracking
SHENZHOU-12202148852U42º39038492Tracking
BD-28199848867U52º41541193Tracking
MIR-SAT 1199848868U52º41340893Tracking
PROGRESS-MS 17202148869U52º42441993Tracking
ISS (NAUKA)202149044U52º42441993Tracking
CYGNUS NG-16202149064U52º42441993Tracking
DRAGON CRS-23202149117U52º42441993Tracking
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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