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)199825544U5242241693Tracking
NSIGHT199842726U5230529791Tracking
KESTREL EYE IIM (KE2M)199842982U5237036492Tracking
ASTERIA199843020U5230630191Tracking
DELLINGR (RBLE)199843021U5236736492Tracking
1KUNS-PF199843466U5232932591Tracking
UBAKUSAT199843467U5236035892Tracking
BATSU-CS1 (IRAZU)199843468U5225524590Tracking
CUBERRT199843546U5236235792Tracking
TEMPEST-D199843547U5238938292Tracking
RAINCUBE199843548U5236635992Tracking
HALOSAT199843549U5236736092Tracking
RADIX199843550U5230729991Tracking
ENDUROSAT ONE199843551U5235534892Tracking
EQUISAT199843552U5236635892Tracking
RADSAT-G199843553U5237536792Tracking
1998-067PC199843554U5235334592Tracking
AEROCUBE 12A201843556U5248347294Tracking
AEROCUBE 12B201843557U5248347394Tracking
LEMUR-2-VU201843558U5247947094Tracking
LEMUR-2-ALEXANDER201843559U5247946994Tracking
LEMUR-2-YUASA201843560U5247947094Tracking
LEMUR-2-TOMHENDERSON201843561U5248047094Tracking
SIRIUSSAT-1199843595U5236536092Tracking
SIRIUSSAT-2199843596U5236636092Tracking
TANUSHA-3199843597U5235134692Tracking
1998-067PK199843598U5235034491Tracking
1998-067PN199843638U5238438192Tracking
1998-067PP199843639U5237637092Tracking
STARS-ME199843640U5238237692Tracking
ISS DEB (SEDA-AP)199843870U5239939492Tracking
CATSAT-2199844029U5238638092Tracking
DELPHINI199844030U5238437892Tracking
UNITE199844031U5239238892Tracking
TECHEDSAT 8199844032U5233232591Tracking
CATSAT-1199844033U5238638092Tracking
ISS DEB199844303U5241040393Tracking
ISS DEB199844304U5239839192Tracking
ISS DEB199844305U5239338792Tracking
ISS DEB199844306U5241140293Tracking
RAAVANA-1199844329U5240439693Tracking
UGUISU199844330U5240539693Tracking
NEPALISAT-1199844331U5240439693Tracking
SPOOQY-1199844332U5240439793Tracking
PINOT199844364U5241240393Tracking
IOD-1 GEMS199844385U5239939592Tracking
SWIATOWID199844426U5239839492Tracking
KRAKSAT199844427U5240640293Tracking
VCC A199844428U5240340093Tracking
ENTRYSAT199844429U5240239893Tracking
VCC C199844430U5240039693Tracking
VCC B199844431U5240440093Tracking
SOYUZ-MS 15201944550U5242241693Tracking
CYGNUS NG-12201944701U5247045594Tracking
ISS DEB199844788U5241340693Tracking
ISS DEB199844789U5241440693Tracking
RWASAT-1199844790U5242140393Tracking
AQT-D199844791U5241441193Tracking
NARSSCUBE-1199844792U5241540893Tracking
PROGRESS-MS 13201944833U5242241693Tracking
STPSAT-4199845043U5242241593Tracking
CYGNUS NG-13202045175U5242241693Tracking
ANTARES DEB202045176U5219615388Tracking
ARGUS-02199845256U5242241293Tracking
AZTECHSAT-1199845257U5242241193Tracking
CRYOCUBE199845258U5242141393Tracking
HARP199845259U5242241293Tracking
PHOENIX199845260U5242241193Tracking
QARMAN199845261U5242241193Tracking
RADSAT-U199845262U5242241293Tracking
SOCRATES199845263U5242241293Tracking
SORTIE199845264U5242341293Tracking
ICS-EF199845265U5242341593Tracking
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 - 2020
Privacy policy