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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)199825544U5242041593Tracking
AEROCUBE 12A201843556U5244143293Tracking
AEROCUBE 12B201843557U5245044093Tracking
LEMUR-2-VU201843558U5240939993Tracking
LEMUR-2-ALEXANDER201843559U5239939192Tracking
LEMUR-2-YUASA201843560U5240239593Tracking
LEMUR-2-TOMHENDERSON201843561U5241440793Tracking
STPSAT-4199845043U5219618588Tracking
ICS-EF (ISS DEB)199845265U5236736192Tracking
RED-EYE 2 (MERLOT)199845800U5232131591Tracking
RED-EYE 3 (CABERNET)199845809U5232131591Tracking
ISS DEB199847853U5240239993Tracking
MMSATS-1199847976U5237637492Tracking
CSS (TIANHE)202148274U4138638392Tracking
ISS DEB199848833U5233933591Tracking
RAMSAT199848850U5226825890Tracking
ISS (NAUKA)202149044U5242041693Tracking
FREGAT DEB201149271U522558832120Tracking
BINAR-1199849272U5214714087Tracking
1998-067TD199851441U5234133291Tracking
PATCOOL199851442U5234133491Tracking
LIGHT-1199851509U5236935792Tracking
PROGRESS-MS 19202251660U5242041693Tracking
IHI-SAT199852147U5236035592Tracking
KITSUNE199852148U5238838592Tracking
CREW DRAGON 4202252318U5242041693Tracking
TIANZHOU-4202252509U4138638392Tracking
PROGRESS-MS 20202252795U5242041693Tracking
SHENZHOU 14202252797U4138638392Tracking
ISS DEB199852952U5238638392Tracking
CSS (WENTIAN)202253239U4138638392Tracking
1998-067TQ199853305U5240239993Tracking
YUZGU 8199853306U5240039693Tracking
1998-067TS199853307U5240039693Tracking
YUZGU 9 (RS3S)199853308U5240039693Tracking
YUZGU 7 (RS1S)199853309U5239939693Tracking
YUZGU 11 (RS5S)199853310U5240039793Tracking
YUZGU 12 (RS6S)199853311U5239939592Tracking
TSIOLKOVSKY-RYAZAN 1 (*)199853312U5239939693Tracking
TSIOLKOVSKY-RYAZAN 2 (*)199853313U5239939693Tracking
YUZGU 10 (RS4S)199853321U5240039693Tracking
YUZGU UA199853322U5240039693Tracking
HSU-SAT1199853462U5240740193Tracking
FUTABA199853463U5240539993Tracking
TUMNANOSAT199853464U5240339793Tracking
1998-067UE199853767U5241140793Tracking
BEAVERCUBE199853768U5241040993Tracking
CLICK-A199853769U5240840693Tracking
1998-067UH199853770U5240740493Tracking
JAGSAT199853771U5240640393Tracking
ISS DEB199853772U5241140793Tracking
SOYUZ-MS 22202253879U5242041693Tracking
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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