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)199825544U5242041293Tracking
AEROCUBE 12A201843556U5244743993Tracking
AEROCUBE 12B201843557U5245444594Tracking
LEMUR-2-VU201843558U5242041393Tracking
LEMUR-2-ALEXANDER201843559U5241640993Tracking
LEMUR-2-YUASA201843560U5241941293Tracking
LEMUR-2-TOMHENDERSON201843561U5242641993Tracking
ISS DEB (SEDA-AP)199843870U5228628190Tracking
STPSAT-4199845043U5231431091Tracking
SORTIE199845264U5229829290Tracking
ICS-EF (ISS DEB)199845265U5237637192Tracking
RED-EYE 2 (MERLOT)199845800U5234334391Tracking
RED-EYE 3 (CABERNET)199845809U5234434291Tracking
ISS DEB199847853U5240540293Tracking
MMSATS-1199847976U5238438392Tracking
CSS (TIANHE)202148274U4138638192Tracking
ISS DEB199848833U5236035892Tracking
RAMSAT199848850U5233332891Tracking
BD-28199848867U5230830091Tracking
ISS (NAUKA)202149044U5242041293Tracking
FREGAT DEB201149271U522456979121Tracking
BINAR-1199849272U5232732391Tracking
CUAVA-1199849275U5228227090Tracking
CAPSAT199849276U5231731191Tracking
PR-CUNAR 2199849277U5228727690Tracking
1998-067TD199851441U5236836292Tracking
PATCOOL199851442U5236736192Tracking
LIGHT-1199851509U5238337492Tracking
PROGRESS-MS 19202251660U5242041293Tracking
SOYUZ-MS 21202252086U5242041293Tracking
IHI-SAT199852147U5238838392Tracking
KITSUNE199852148U5239939392Tracking
CREW DRAGON 4202252318U5242041293Tracking
TIANZHOU-4202252509U4138638192Tracking
PROGRESS-MS 20202252795U5242041293Tracking
SHENZHOU 14202252797U4138638192Tracking
ISS DEB199852952U5240840293Tracking
DRAGON CRS-25202253113U5242041293Tracking
CSS (WENTIAN)202253239U4138638192Tracking
1998-067TQ199853305U5241541093Tracking
1998-067TR199853306U5241441093Tracking
1998-067TS199853307U5241441093Tracking
RS3S199853308U5241441093Tracking
RS1S199853309U5241440993Tracking
RS5S199853310U5241441093Tracking
RS6S199853311U5241341093Tracking
RS9S199853312U5241440993Tracking
RS12S199853313U5241440993Tracking
RS4S199853321U5241441093Tracking
1998-067UA199853322U5241441093Tracking
1998-067UB199853462U5241940893Tracking
1998-067UC199853463U5241940893Tracking
1998-067UD199853464U5241940893Tracking
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