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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)199825544U5242341793Tracking
AEROCUBE 12A201843556U5247246394Tracking
AEROCUBE 12B201843557U5247446594Tracking
LEMUR-2-VU201843558U5246345594Tracking
LEMUR-2-ALEXANDER201843559U5246245594Tracking
LEMUR-2-YUASA201843560U5246345594Tracking
LEMUR-2-TOMHENDERSON201843561U5246545794Tracking
ISS DEB (SEDA-AP)199843870U5237537092Tracking
UNITE199844031U5219819288Tracking
ISS DEB199844303U5238337692Tracking
ISS DEB199844306U5238137292Tracking
RED-EYE 1 (PINOT)199844364U5238537692Tracking
KRAKSAT199844427U5233933291Tracking
VCC A199844428U5215214587Tracking
RWASAT-1199844790U5237936992Tracking
AQT-D199844791U5237736892Tracking
NARSSCUBE-1199844792U5233232391Tracking
STPSAT-4199845043U5240039492Tracking
HARP199845256U5237937092Tracking
1998-067RA199845257U5238537692Tracking
PHOENIX199845258U5239138392Tracking
1998-067RC199845259U5236135292Tracking
CRYOCUBE199845260U5232431291Tracking
AZTECHSAT-1199845261U5233232091Tracking
RADSAT-U199845262U5238237592Tracking
QARMAN199845263U5236135292Tracking
SORTIE199845264U5239939092Tracking
ICS-EF (ISS DEB)199845265U5240940293Tracking
G-SAT199845597U5238137792Tracking
QUETZAL-1199845598U5236836592Tracking
RED-EYE 2 (MERLOT)199845800U5240140093Tracking
RED-EYE 3 (CABERNET)199845809U5240240093Tracking
DEMI199845916U5237537092Tracking
SPOC199846921U5239439392Tracking
BOBCAT-1199846922U5238438292Tracking
NEUTRON-1199846923U5239539392Tracking
1998-067RU199846924U5235534892Tracking
LEMUR-2-BAXTER-OLIVER199846925U5234734191Tracking
LEMUR-2-DJARA199846926U5235735192Tracking
DESCENT199846927U5239539392Tracking
ISS DEB199847853U5241841493Tracking
RSP-01199847925U5240240193Tracking
TAUSAT-1199847926U5239839692Tracking
TSURU199847927U5240440293Tracking
STARS-EC199847928U5240139493Tracking
MMSATS-1199847976U5241541293Tracking
CREW DRAGON 2202148209U5242341793Tracking
TIANHE202148274U4139038192Tracking
TIANZHOU-2202148803U4139038192Tracking
RAMSAT199848850U5241440893Tracking
SOAR199848851U5239839192Tracking
BD-28199848867U5241240893Tracking
MIR-SAT 1199848868U5240640293Tracking
PROGRESS-MS 17202148869U5242341793Tracking
ISS (NAUKA)202149044U5242341793Tracking
CYGNUS NG-16202149064U5242341793Tracking
DRAGON CRS-23 DEB202149268U5235724291Tracking
SOYUZ-MS 19202149269U5242341793Tracking
FREGAT DEB201149271U5225221148123Tracking
1998-067SR199849272U5241941293Tracking
MAYA-3199849273U5241941293Tracking
MAYA-4199849274U5241941393Tracking
CUAVA-1199849275U5241941293Tracking
CAPSAT199849276U5242141493Tracking
1998-067SW199849277U5242141393Tracking
1998-067SX199849278U5242041293Tracking
SHENZHOU-13 (SZ-13)202149326U4139038192Tracking
CZ-2F R/B202149327U4129118689Tracking
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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