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)199825544U5242241793Tracking
KESTREL EYE IIM (KE2M)199842982U5232231891Tracking
DELLINGR (RBLE)199843021U5231130991Tracking
TEMPEST-D199843547U5233733391Tracking
RADSAT-G199843553U5228728290Tracking
AEROCUBE 12A201843556U5247846794Tracking
AEROCUBE 12B201843557U5248046894Tracking
LEMUR-2-VU201843558U5247246294Tracking
LEMUR-2-ALEXANDER201843559U5247246194Tracking
LEMUR-2-YUASA201843560U5247246294Tracking
LEMUR-2-TOMHENDERSON201843561U5247346394Tracking
1998-067PN199843638U5234734591Tracking
1998-067PP199843639U5225024689Tracking
STARS-ME199843640U5233132891Tracking
ISS DEB (SEDA-AP)199843870U5238838392Tracking
CATSAT-2199844029U5230530091Tracking
DELPHINI199844030U5225625190Tracking
UNITE199844031U5235935592Tracking
CATSAT-1199844033U5230530091Tracking
ISS DEB199844303U5239739192Tracking
ISS DEB199844304U5227827390Tracking
ISS DEB199844306U5239739092Tracking
RAAVANA-1199844329U5236736292Tracking
UGUISU199844330U5236736392Tracking
NEPALISAT-1199844331U5236736292Tracking
SPOOQY-1199844332U5236836492Tracking
RED-EYE 1 (PINOT)199844364U5239939192Tracking
IOD-1 GEMS199844385U5231130791Tracking
SWIATOWID199844426U5226726190Tracking
KRAKSAT199844427U5238137992Tracking
VCC A199844428U5236936792Tracking
ENTRYSAT199844429U5235735692Tracking
VCC C199844430U5233733391Tracking
VCC B199844431U5236836692Tracking
ISS DEB199844788U5234634391Tracking
ISS DEB199844789U5235635192Tracking
RWASAT-1199844790U5240039192Tracking
AQT-D199844791U5239939292Tracking
NARSSCUBE-1199844792U5238738292Tracking
STPSAT-4199845043U5241240593Tracking
HARP199845256U5240339593Tracking
1998-067RA199845257U5240639793Tracking
PHOENIX199845258U5240740093Tracking
1998-067RC199845259U5239839192Tracking
CRYOCUBE199845260U5239738992Tracking
AZTECHSAT-1199845261U5239338592Tracking
RADSAT-U199845262U5240539793Tracking
QARMAN199845263U5239939192Tracking
SORTIE199845264U5241140293Tracking
ICS-EF (ISS DEB)199845265U5241540993Tracking
PROGRESS-MS 14202045595U5242241793Tracking
G-SAT199845597U5240539993Tracking
QUETZAL-1199845598U5240139793Tracking
RED-EYE 2 (MERLOT)199845800U5241141093Tracking
RED-EYE 3 (CABERNET)199845809U5241141093Tracking
DEMI199845916U5240340193Tracking
TECHEDSAT 10199845917U5229728790Tracking
SOYUZ-MS 17202046613U5242241793Tracking
CREW DRAGON 1202046920U5242241793Tracking
SPOC199846921U5241240893Tracking
BOBCAT-1199846922U5240940693Tracking
NEUTRON-1199846923U5241240893Tracking
1998-067RU199846924U5240440293Tracking
LEMUR-2-BAXTER-OLIVER199846925U5240340093Tracking
LEMUR-2-DJARA199846926U5240440193Tracking
DESCENT199846927U5241240993Tracking
PROGRESS-MS 16202147618U5242241793Tracking
CYGNUS NG-15202147689U5242241793Tracking
ANTARES R/B202147690U5215713787Tracking
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