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Scientific Satellites
Below follows the information found in the database of scientific satellites. They are satellites placed in orbit in order to study the high-atmosphere, effects of cosmic radiation or specific natural resources. In this category also are the telescopes and space observatories.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
Hubble199020580U28º51050695Tracking
POLAR199623802U79º5012780981109Tracking
SWAS199825560U70º56755796Tracking
CXO199925867U43º14549433243809Tracking
XMM-NEWTON199925989U67º94433266682872Tracking
TERRA199925994U98º69569199Tracking
CLUSTER II-FM7 (SAMBA)200026410U140º122473102953256Tracking
CLUSTER II-FM5 (RUMBA)200026463U152º13274230163356Tracking
CLUSTER II-FM8 (TANGO)200026464U140º122489103013256Tracking
ODIN200126702U97º49248394Tracking
TIMED200126998U74º59259197Tracking
INTEGRAL200227540U90º14477247163832Tracking
CORIOLIS200327640U99º836817101Tracking
SORCE200327651U40º59256496Tracking
MOST200327843U99º828815101Tracking
SCISAT 1200327858U74º63662597Tracking
SWIFT200428485U21º50349495Tracking
CALIPSO200629108U98º67467198Tracking
HINODE (SOLAR-B)200629479U98º68465898Tracking
SHIJIAN-6 02A (SJ-6 02A)200629505U98º55454896Tracking
SHIJIAN-6 02B (SJ-6 02B)200629506U98º57557196Tracking
FGRST (GLAST)200833053U26º51950695Tracking
SDO201036395U33º35790357801436Tracking
CRYOSAT 2201036508U92º72271799Tracking
X-SAT201137389U98º820798101Tracking
GCOM-W1 (SHIZUKU)201238337U98º70470199Tracking
NUSTAR201238358U58356896Tracking
NEOSSAT201339089U98º782766100Tracking
BRITE-AUSTRIA201339091U98º780764100Tracking
IRIS201339197U98º63860497Tracking
HISAKI (SPRINT-A)201339253U30º1154951106Tracking
CASSIOPE201339265U81º97730998Tracking
STSAT-3201339422U98º59556496Tracking
SWARM B201339451U88º50449995Tracking
SWARM A201339452U87º46546094Tracking
SWARM C201339453U87º46546094Tracking
BRITE-CA1 (TORONTO)201440020U98º71960398Tracking
OCO 2201440059U98º70470199Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º61058797Tracking
RESURS-P 2201440360U97º37036592Tracking
MMS 1201540482U53º17952730235062Tracking
MMS 2201540483U53º17954330235062Tracking
MMS 3201540484U53º17954230235062Tracking
MMS 4201540485U53º17969730295069Tracking
ASTROSAT201540930U63762597Tracking
DAMPE201541173U97º49147494Tracking
PISAT201641784U98º69565098Tracking
HXMT (HUIYAN)201742758U43º52550795Tracking
FLYING LAPTOP201742831U97º58957096Tracking
ZHANGHENG 1 (CSES)201843194U98º50849895Tracking
SALSAT202046495U98º53151195Tracking
IXPE202149954U57456196Tracking
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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