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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)199825544U5242441993Tracking
KESTREL EYE IIM (KE2M)199842982U5214814387Tracking
AEROCUBE 12A201843556U5247446394Tracking
AEROCUBE 12B201843557U5247646594Tracking
LEMUR-2-VU201843558U5246645694Tracking
LEMUR-2-ALEXANDER201843559U5246545694Tracking
LEMUR-2-YUASA201843560U5246645694Tracking
LEMUR-2-TOMHENDERSON201843561U5246845794Tracking
1998-067PN199843638U5223122089Tracking
ISS DEB (SEDA-AP)199843870U5237837492Tracking
UNITE199844031U5229529290Tracking
ISS DEB199844303U5238638192Tracking
ISS DEB199844306U5238437892Tracking
RAAVANA-1199844329U5227827290Tracking
UGUISU199844330U5228628190Tracking
NEPALISAT-1199844331U5228027490Tracking
SPOOQY-1199844332U5229228890Tracking
RED-EYE 1 (PINOT)199844364U5238738192Tracking
KRAKSAT199844427U5235134892Tracking
VCC A199844428U5230329991Tracking
VCC B199844431U5229729290Tracking
RWASAT-1199844790U5238337792Tracking
AQT-D199844791U5238237692Tracking
NARSSCUBE-1199844792U5234834791Tracking
STPSAT-4199845043U5240239793Tracking
HARP199845256U5238437992Tracking
1998-067RA199845257U5238938392Tracking
PHOENIX199845258U5239438992Tracking
1998-067RC199845259U5237036692Tracking
CRYOCUBE199845260U5235034892Tracking
AZTECHSAT-1199845261U5235034892Tracking
RADSAT-U199845262U5238738292Tracking
QARMAN199845263U5237036692Tracking
SORTIE199845264U5240139493Tracking
ICS-EF (ISS DEB)199845265U5241040493Tracking
G-SAT199845597U5238738392Tracking
QUETZAL-1199845598U5237837592Tracking
RED-EYE 2 (MERLOT)199845800U5240340393Tracking
RED-EYE 3 (CABERNET)199845809U5240340393Tracking
DEMI199845916U5238237992Tracking
SPOC199846921U5240039693Tracking
BOBCAT-1199846922U5239238892Tracking
NEUTRON-1199846923U5240039693Tracking
1998-067RU199846924U5237236792Tracking
LEMUR-2-BAXTER-OLIVER199846925U5236736292Tracking
LEMUR-2-DJARA199846926U5237336992Tracking
DESCENT199846927U5240039693Tracking
ISS DEB199847853U5241941593Tracking
RSP-01199847925U5240840493Tracking
TAUSAT-1199847926U5240540093Tracking
TSURU199847927U5240940593Tracking
STARS-EC199847928U5240839993Tracking
MMSATS-1199847976U5241741393Tracking
SOYUZ-MS 18202148159U5242441993Tracking
CREW DRAGON 2202148209U5242441993Tracking
TIANHE202148274U4138638092Tracking
TIANZHOU-2202148803U4138638192Tracking
RAMSAT199848850U5241741093Tracking
SOAR199848851U5240840193Tracking
SHENZHOU-12202148852U4239038492Tracking
BD-28199848867U5241541193Tracking
MIR-SAT 1199848868U5241340893Tracking
PROGRESS-MS 17202148869U5242441993Tracking
ISS (NAUKA)202149044U5242441993Tracking
CYGNUS NG-16202149064U5242441993Tracking
DRAGON CRS-23202149117U5242441993Tracking
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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