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)199825544U52º42341793Tracking
AEROCUBE 12A201843556U52º47246394Tracking
AEROCUBE 12B201843557U52º47446594Tracking
LEMUR-2-VU201843558U52º46345594Tracking
LEMUR-2-ALEXANDER201843559U52º46245594Tracking
LEMUR-2-YUASA201843560U52º46345594Tracking
LEMUR-2-TOMHENDERSON201843561U52º46545794Tracking
ISS DEB (SEDA-AP)199843870U52º37537092Tracking
UNITE199844031U52º19819288Tracking
ISS DEB199844303U52º38337692Tracking
ISS DEB199844306U52º38137292Tracking
RED-EYE 1 (PINOT)199844364U52º38537692Tracking
KRAKSAT199844427U52º33933291Tracking
VCC A199844428U52º15214587Tracking
RWASAT-1199844790U52º37936992Tracking
AQT-D199844791U52º37736892Tracking
NARSSCUBE-1199844792U52º33232391Tracking
STPSAT-4199845043U52º40039492Tracking
HARP199845256U52º37937092Tracking
1998-067RA199845257U52º38537692Tracking
PHOENIX199845258U52º39138392Tracking
1998-067RC199845259U52º36135292Tracking
CRYOCUBE199845260U52º32431291Tracking
AZTECHSAT-1199845261U52º33232091Tracking
RADSAT-U199845262U52º38237592Tracking
QARMAN199845263U52º36135292Tracking
SORTIE199845264U52º39939092Tracking
ICS-EF (ISS DEB)199845265U52º40940293Tracking
G-SAT199845597U52º38137792Tracking
QUETZAL-1199845598U52º36836592Tracking
RED-EYE 2 (MERLOT)199845800U52º40140093Tracking
RED-EYE 3 (CABERNET)199845809U52º40240093Tracking
DEMI199845916U52º37537092Tracking
SPOC199846921U52º39439392Tracking
BOBCAT-1199846922U52º38438292Tracking
NEUTRON-1199846923U52º39539392Tracking
1998-067RU199846924U52º35534892Tracking
LEMUR-2-BAXTER-OLIVER199846925U52º34734191Tracking
LEMUR-2-DJARA199846926U52º35735192Tracking
DESCENT199846927U52º39539392Tracking
ISS DEB199847853U52º41841493Tracking
RSP-01199847925U52º40240193Tracking
TAUSAT-1199847926U52º39839692Tracking
TSURU199847927U52º40440293Tracking
STARS-EC199847928U52º40139493Tracking
MMSATS-1199847976U52º41541293Tracking
CREW DRAGON 2202148209U52º42341793Tracking
TIANHE202148274U41º39038192Tracking
TIANZHOU-2202148803U41º39038192Tracking
RAMSAT199848850U52º41440893Tracking
SOAR199848851U52º39839192Tracking
BD-28199848867U52º41240893Tracking
MIR-SAT 1199848868U52º40640293Tracking
PROGRESS-MS 17202148869U52º42341793Tracking
ISS (NAUKA)202149044U52º42341793Tracking
CYGNUS NG-16202149064U52º42341793Tracking
DRAGON CRS-23 DEB202149268U52º35724291Tracking
SOYUZ-MS 19202149269U52º42341793Tracking
FREGAT DEB201149271U52º25221148123Tracking
1998-067SR199849272U52º41941293Tracking
MAYA-3199849273U52º41941293Tracking
MAYA-4199849274U52º41941393Tracking
CUAVA-1199849275U52º41941293Tracking
CAPSAT199849276U52º42141493Tracking
1998-067SW199849277U52º42141393Tracking
1998-067SX199849278U52º42041293Tracking
SHENZHOU-13 (SZ-13)202149326U41º39038192Tracking
CZ-2F R/B202149327U41º29118689Tracking
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 - 2021
Privacy policy