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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)199825544U5240839993Tracking
TIANGONG 1201137820U4336133892Tracking
SPINSAT199840314U5223923089Tracking
AGGIESAT 4199841313U5236536192Tracking
BEVO 2199841314U5233032891Tracking
MINXSS199841474U5233433191Tracking
STMSAT-1199841476U5232632191Tracking
NODES 2199841477U5235935692Tracking
NODES 1199841478U5236035792Tracking
FLOCK 2E'-1199841479U5237637492Tracking
FLOCK 2E'-3199841480U5237637392Tracking
FLOCK 2E'-2199841481U5237437192Tracking
FLOCK 2E'-4199841482U5237237092Tracking
FLOCK 2E-1199841483U5237737592Tracking
FLOCK 2E-2199841484U5237437392Tracking
LEMUR-2-THERESACONDOR199841485U5230629991Tracking
FLOCK 2E-3199841486U5237937792Tracking
FLOCK 2E-4199841487U5237637592Tracking
LEMUR-2-NICK-ALLAIN199841488U5231430991Tracking
LEMUR-2-KANE199841489U5231531091Tracking
LEMUR-2-JEFF199841490U5229729090Tracking
FLOCK 2E-6199841563U5238037792Tracking
FLOCK 2E-5199841564U5238037792Tracking
FLOCK 2E-7199841565U5237537192Tracking
FLOCK 2E-8199841566U5234834691Tracking
FLOCK 2E'-5199841567U5238337892Tracking
FLOCK 2E'-6199841568U5237937592Tracking
FLOCK 2E'-8199841569U5237337292Tracking
FLOCK 2E'-7199841570U5236936892Tracking
FLOCK 2E-9199841571U5237337092Tracking
FLOCK 2E-10199841572U5237737292Tracking
FLOCK 2E-12199841573U5237537192Tracking
FLOCK 2E-11199841574U5237537092Tracking
FLOCK 2E'-9199841575U5237336992Tracking
FLOCK 2E'-10199841576U5237637192Tracking
FLOCK 2E'-11199841577U5237737192Tracking
FLOCK 2E'-12199841578U5237537092Tracking
FLOCK 2E'-13199841761U5239838792Tracking
FLOCK 2E'-14199841762U5239738892Tracking
FLOCK 2E'-16199841763U5239738792Tracking
FLOCK 2E'-15199841764U5239838892Tracking
TIANGONG-2201641765U4337736892Tracking
FLOCK 2E'-18199841769U5239738992Tracking
FLOCK 2E'-17199841776U5239738892Tracking
FLOCK 2E'-19199841777U5239238592Tracking
FLOCK 2E'-20199841782U5239338692Tracking
SOYUZ-MS 02201641820U5240839993Tracking
BANXING-2201641834U4337736892Tracking
SOYUZ-MS 03201641864U5240839993Tracking
STARS-C199841895U5240239493Tracking
TANCREDO-1199841931U5240238992Tracking
ITF-2199841932U5240539593Tracking
WASEDA-SAT3199841933U5240539493Tracking
EGG199841934U5240238792Tracking
AOBA-VELOX 3199841935U5240539593Tracking
TUPOD199841936U5240038992Tracking
OSNSAT199841939U5240339193Tracking
DRAGON CRS-10201742053U5240839993Tracking
PROGRESS-MS 05201742056U5240839993Tracking
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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