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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)199825544U5242341593Tracking
NSIGHT199842726U5231531291Tracking
KESTREL EYE IIM (KE2M)199842982U5237136792Tracking
ASTERIA199843020U5231631491Tracking
DELLINGR (RBLE)199843021U5236836692Tracking
1KUNS-PF199843466U5233733591Tracking
UBAKUSAT199843467U5236436192Tracking
BATSU-CS1 (IRAZU)199843468U5229729290Tracking
CUBERRT199843546U5236336092Tracking
TEMPEST-D199843547U5238938392Tracking
RAINCUBE199843548U5236836392Tracking
HALOSAT199843549U5236936492Tracking
RADIX199843550U5232231991Tracking
ENDUROSAT ONE199843551U5235935492Tracking
EQUISAT199843552U5236836392Tracking
1998-067PB199843553U5237637092Tracking
1998-067PC199843554U5235635292Tracking
AEROCUBE 12A201843556U5248447294Tracking
AEROCUBE 12B201843557U5248447294Tracking
LEMUR-2-VU201843558U5248046994Tracking
LEMUR-2-ALEXANDER201843559U5248046994Tracking
LEMUR-2-YUASA201843560U5248147094Tracking
LEMUR-2-TOMHENDERSON201843561U5248147094Tracking
SIRIUSSAT-1199843595U5236836592Tracking
SIRIUSSAT-2199843596U5236836592Tracking
TANUSHA-3199843597U5235635392Tracking
1998-067PK199843598U5235435292Tracking
1998-067PN199843638U5238538392Tracking
1998-067PP199843639U5237837392Tracking
STARS-ME199843640U5238437892Tracking
ISS DEB (SEDA-AP)199843870U5239939593Tracking
CATSAT-2199844029U5238738292Tracking
DELPHINI199844030U5238538192Tracking
UNITE199844031U5239339092Tracking
TECHEDSAT 8199844032U5234434191Tracking
CATSAT-1199844033U5238738392Tracking
ISS DEB199844303U5241140393Tracking
ISS DEB199844304U5240139392Tracking
ISS DEB199844305U5239639092Tracking
ISS DEB199844306U5241340393Tracking
RAAVANA-1199844329U5240639793Tracking
UGUISU199844330U5240639793Tracking
NEPALISAT-1199844331U5240639793Tracking
SPOOQY-1199844332U5240539893Tracking
PINOT199844364U5241340393Tracking
IOD-1 GEMS199844385U5240239793Tracking
SWIATOWID199844426U5240139693Tracking
KRAKSAT199844427U5240840293Tracking
VCC A199844428U5240540193Tracking
ENTRYSAT199844429U5240440093Tracking
VCC C199844430U5240339893Tracking
VCC B199844431U5240540193Tracking
SOYUZ-MS 13201944437U5242341593Tracking
SOYUZ-MS 15201944550U5242341593Tracking
CYGNUS NG-12201944701U5242341593Tracking
ISS DEB199844788U5241540893Tracking
ISS DEB199844789U5241740793Tracking
RWASAT-1199844790U5241840793Tracking
AQT-D199844791U5241641193Tracking
NARSSCUBE-1199844792U5241640993Tracking
DRAGON CRS-19201944821U5242241493Tracking
PROGRESS-MS 13201944833U5242341593Tracking
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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