Brazil  Portugal  English
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)199825544U5242041493Tracking
AEROCUBE 12A201843556U5242841793Tracking
AEROCUBE 12B201843557U5244043093Tracking
LEMUR-2-VU201843558U5237536392Tracking
LEMUR-2-ALEXANDER201843559U5234533191Tracking
LEMUR-2-YUASA201843560U5235534192Tracking
LEMUR-2-TOMHENDERSON201843561U5238737692Tracking
ICS-EF (ISS DEB)199845265U5234633991Tracking
ISS DEB [EP BATTERY]199847853U5239639492Tracking
MMSATS-1199847976U5235835592Tracking
CSS (TIANHE)202148274U4139338692Tracking
ISS (NAUKA)202149044U5242041493Tracking
FREGAT DEB201149271U522501868120Tracking
LIGHT-1199851509U5232531291Tracking
KITSUNE199852148U5237036092Tracking
PROGRESS-MS 20202252795U5242041493Tracking
ISS DEB199852952U5229928590Tracking
CSS (WENTIAN)202253239U4139338692Tracking
1998-067TQ199853305U5237436392Tracking
YUZGU 8199853306U5236335292Tracking
1998-067TS199853307U5236435392Tracking
YUZGU 9 (RS3S)199853308U5236535492Tracking
YUZGU 7 (RS1S)199853309U5236435292Tracking
YUZGU 11 (RS5S)199853310U5236535492Tracking
YUZGU 12 (RS6S)199853311U5236135092Tracking
TSIOLKOVSKY-RYAZAN 1 (*)199853312U5236535392Tracking
TSIOLKOVSKY-RYAZAN 2 (*)199853313U5236435392Tracking
YUZGU 10 (RS4S)199853321U5236435392Tracking
YUZGU UA199853322U5236335292Tracking
HSU-SAT1199853462U5238637392Tracking
FUTABA199853463U5237836592Tracking
TUMNANOSAT199853464U5237035592Tracking
1998-067UE199853767U5239538792Tracking
BEAVERCUBE199853768U5239538892Tracking
CLICK-A199853769U5238437692Tracking
1998-067UH199853770U5237236092Tracking
JAGSAT199853771U5236835592Tracking
ISS DEB199853772U5238837692Tracking
SOYUZ-MS 22202253879U5242041493Tracking
CREW DRAGON 5202253963U5242041493Tracking
PROGRESS-MS 21202254155U5242041493Tracking
CSS (MENGTIAN)202254216U4139338692Tracking
CYGNUS NG-18202254232U5242041493Tracking
TIANZHOU-5202254237U4139338692Tracking
DRAGON CRS-26202254371U5242041493Tracking
SHENZHOU-15202254379U4139338692Tracking
2022-162B202254380U4128218289Tracking
1998-067UL199854534U5242040993Tracking
1998-067UM199854535U5242040993Tracking
1998-067UN199854536U5242040993Tracking
1998-067UP199854537U5242040993Tracking
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.

Satview - All Rights Reserved 2008 - 2022
Privacy policy