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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)199825544U5242141293Tracking
AEROCUBE 12A201843556U5243242193Tracking
AEROCUBE 12B201843557U5244343293Tracking
LEMUR-2-VU201843558U5238837592Tracking
LEMUR-2-ALEXANDER201843559U5236935792Tracking
LEMUR-2-YUASA201843560U5237536392Tracking
LEMUR-2-TOMHENDERSON201843561U5239938592Tracking
ICS-EF (ISS DEB)199845265U5235434692Tracking
RED-EYE 2 (MERLOT)199845800U5219919488Tracking
RED-EYE 3 (CABERNET)199845809U5217917588Tracking
ISS DEB199847853U5239739592Tracking
MMSATS-1199847976U5236536192Tracking
CSS (TIANHE)202148274U4139438192Tracking
ISS DEB199848833U5228827990Tracking
ISS (NAUKA)202149044U5242141293Tracking
FREGAT DEB201149271U522527846120Tracking
1998-067TD199851441U5222221489Tracking
PATCOOL199851442U5224523589Tracking
LIGHT-1199851509U5234433091Tracking
IHI-SAT199852147U5225624490Tracking
KITSUNE199852148U5237736892Tracking
TIANZHOU-4202252509U4139337492Tracking
PROGRESS-MS 20202252795U5242141293Tracking
SHENZHOU 14202252797U4139438192Tracking
ISS DEB199852952U5234633291Tracking
CSS (WENTIAN)202253239U4139438192Tracking
1998-067TQ199853305U5238637592Tracking
YUZGU 8199853306U5237936892Tracking
1998-067TS199853307U5237936892Tracking
YUZGU 9 (RS3S)199853308U5238036992Tracking
YUZGU 7 (RS1S)199853309U5237936792Tracking
YUZGU 11 (RS5S)199853310U5238036992Tracking
YUZGU 12 (RS6S)199853311U5237836692Tracking
TSIOLKOVSKY-RYAZAN 1 (*)199853312U5237936892Tracking
TSIOLKOVSKY-RYAZAN 2 (*)199853313U5237936892Tracking
YUZGU 10 (RS4S)199853321U5237936892Tracking
YUZGU UA199853322U5237936792Tracking
HSU-SAT1199853462U5239538292Tracking
FUTABA199853463U5238937592Tracking
TUMNANOSAT199853464U5238336992Tracking
1998-067UE199853767U5240139393Tracking
BEAVERCUBE199853768U5240039493Tracking
CLICK-A199853769U5239438692Tracking
1998-067UH199853770U5238637592Tracking
JAGSAT199853771U5238437292Tracking
ISS DEB199853772U5239738592Tracking
SOYUZ-MS 22202253879U5242141293Tracking
CREW DRAGON 5202253963U5242141293Tracking
PROGRESS-MS 21202254155U5242141293Tracking
MENGTIAN202254216U4139438192Tracking
CYGNUS NG-18202254232U5242141293Tracking
TIANZHOU-5202254237U4139438192Tracking
2022-152B202254238U4238319290Tracking
2022-152C202254239U4234519290Tracking
CZ-7 R/B202254240U4120618688Tracking
2022-152E202254241U4132917690Tracking
2022-152F202254242U41604-9190Tracking
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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