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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
Hubble199020580U28º51651395Tracking
POLAR199623802U79º4989383311109Tracking
SWAS199825560U70º57256396Tracking
CXO199925867U40º14655322593808Tracking
XMM-NEWTON199925989U68º95441256712872Tracking
TERRA199925994U98º69669299Tracking
CLUSTER II-FM7 (SAMBA)200026410U139º120065127623258Tracking
CLUSTER II-FM6 (SALSA)200026411U148º13137513753255Tracking
CLUSTER II-FM5 (RUMBA)200026463U150º12796248323256Tracking
CLUSTER II-FM8 (TANGO)200026464U139º120088127083256Tracking
ODIN200126702U97º50949595Tracking
TIMED200126998U74º59459497Tracking
INTEGRAL200227540U89º14503444463832Tracking
CORIOLIS200327640U99º836818101Tracking
SORCE200327651U40º59956896Tracking
MOST200327843U99º829815101Tracking
SCISAT 1200327858U74º63762797Tracking
SWIFT200428485U21º51850695Tracking
CALIPSO200629108U98º67667498Tracking
HINODE (SOLAR-B)200629479U98º68566198Tracking
SHIJIAN-6 02A (SJ-6 02A)200629505U98º56055796Tracking
SHIJIAN-6 02B (SJ-6 02B)200629506U98º57857396Tracking
FGRST (GLAST)200833053U26º52451095Tracking
WISE200936119U97º38938892Tracking
SDO201036395U33º35793357791436Tracking
CRYOSAT 2201036508U92º72371699Tracking
X-SAT201137389U98º821798101Tracking
GCOM-W1 (SHIZUKU)201238337U98º70470199Tracking
NUSTAR201238358U58857396Tracking
NEOSSAT201339089U98º783766100Tracking
BRITE-AUSTRIA201339091U98º780765100Tracking
IRIS201339197U98º64160697Tracking
HISAKI (SPRINT-A)201339253U30º1154951106Tracking
CASSIOPE201339265U81º102331198Tracking
STSAT-3201339422U98º59956896Tracking
SWARM B201339451U88º50850495Tracking
SWARM A201339452U87º47246994Tracking
SWARM C201339453U87º47246994Tracking
BRITE-CA1 (TORONTO)201440020U98º72260598Tracking
OCO 2201440059U98º70470199Tracking
BRITE-PL2 (HEWELIUSZ)201440119U98º61459197Tracking
RESURS-P 2201440360U97º40339293Tracking
MMS 1201540482U45º18084822055081Tracking
MMS 2201540483U45º18086721985082Tracking
MMS 3201540484U45º18085421995081Tracking
MMS 4201540485U45º18084322105081Tracking
ASTROSAT201540930U63962797Tracking
DAMPE201541173U97º49347794Tracking
PISAT201641784U98º69765298Tracking
HXMT (HUIYAN)201742758U43º53651495Tracking
FLYING LAPTOP201742831U97º59157596Tracking
ZHANGHENG 1 (CSES)201843194U98º50849995Tracking
SALSAT202046495U98º54051895Tracking
IXPE202149954U58156796Tracking
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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