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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)199825544U5242141293Tracking
ALTAIR PATHFINDER199842711U5225625190Tracking
NSIGHT199842726U5233532991Tracking
KESTREL EYE IIM (KE2M)199842982U5237537092Tracking
ASTERIA199843020U5233433291Tracking
DELLINGR (RBLE)199843021U5237237092Tracking
1KUNS-PF199843466U5235134892Tracking
UBAKUSAT199843467U5236936892Tracking
BATSU-CS1 (IRAZU)199843468U5233232791Tracking
CUBERRT199843546U5236836292Tracking
TEMPEST-D199843547U5239238592Tracking
RAINCUBE199843548U5237636992Tracking
HALOSAT199843549U5237636992Tracking
RADIX199843550U5234734091Tracking
ENDUROSAT ONE199843551U5236936192Tracking
EQUISAT199843552U5237636892Tracking
1998-067PB199843553U5238237392Tracking
1998-067PC199843554U5236735992Tracking
AEROCUBE 12A201843556U5248447394Tracking
AEROCUBE 12B201843557U5248447394Tracking
LEMUR-2-VU201843558U5248147194Tracking
LEMUR-2-ALEXANDER201843559U5248047194Tracking
LEMUR-2-YUASA201843560U5248147194Tracking
LEMUR-2-TOMHENDERSON201843561U5248147194Tracking
SIRIUSSAT-1199843595U5237537192Tracking
SIRIUSSAT-2199843596U5237537192Tracking
TANUSHA-3199843597U5236736292Tracking
1998-067PK199843598U5236636192Tracking
1998-067PN199843638U5238938692Tracking
1998-067PP199843639U5238337892Tracking
STARS-ME199843640U5238838292Tracking
ISS DEB (SEDA-AP)199843870U5240139693Tracking
CATSAT-2199844029U5239338692Tracking
DELPHINI199844030U5239238592Tracking
UNITE199844031U5239739292Tracking
TECHEDSAT 8199844032U5236636092Tracking
CATSAT-1199844033U5239338692Tracking
CYGNUS NG-11201944188U5247046294Tracking
ISS DEB199844303U5241240593Tracking
ISS DEB199844304U5240539993Tracking
ISS DEB199844305U5240239693Tracking
ISS DEB199844306U5241440593Tracking
RAAVANA-1199844329U5240940193Tracking
UGUISU199844330U5240940193Tracking
NEPALISAT-1199844331U5240940093Tracking
SPOOQY-1199844332U5240840193Tracking
PINOT199844364U5241440593Tracking
IOD-1 GEMS199844385U5240540293Tracking
SWIATOWID199844426U5240540293Tracking
KRAKSAT199844427U5241040693Tracking
VCC A199844428U5240840593Tracking
ENTRYSAT199844429U5240740493Tracking
VCC C199844430U5240640393Tracking
VCC B199844431U5240840593Tracking
SOYUZ-MS 13201944437U5242141293Tracking
PROGRESS-MS 12201944455U5242141293Tracking
SOYUZ-MS 15201944550U5242141293Tracking
CYGNUS NG-12201944701U5242141293Tracking
1998-067QT199844788U5241941293Tracking
1998-067QU199844789U5242041193Tracking
OBJECT QV199844790U5241941093Tracking
OBJECT QW199844791U5241741293Tracking
OBJECT QX199844792U5241941293Tracking
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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