Şablon:Gemiya Azmini

Wikipediya ra ensiklopediya xosere
Xıl de be pusula Xıl de cıgeyrayışi
[bıvurne] Dokumantasyon


Usage[çımey bıvurnê]

{{Infobox spacecraft
| name                   = 
| image                  = 
| caption                =
| mission_identifier     =

| organisation           = 
| major_contractors      = 
| bus                    = 
| mission_type           = 
| flyby_of               = 
| flyby_date             = 
| current_destination    = 
| satellite_of           = 
| orbital_insertion_date = 
| orbits                 = 
| launch_date            = 
| launch_vehicle         =
| carrier_rocket         = <!-- or American "launch_vehicle" can be used -->
| flight_number          = 
| launch_site            = 
| mission_duration       = 

| mission_highlight      = 
| decay                  =
| return                 = <!-- for spacecraft designed to return to Earth -->
| return_site            = <!-- for spacecraft designed to return to Earth -->

| nolink                 = <!-- set to anything to prevent linking COSPAR to NSSDC database -->
| COSPAR_ID              = <!-- designations for pre-1963 launches should include a Greek letter, launches that failed to reach any orbit should not have a COSPAR -->
| NSSDC_ID               = 
| webpage                = 
| mass                   = 
| dimensions             = 
| power                  = 
| batteries              = 

<!-- Orbit data -->
| orbit_reference        = <!-- reference system -->
| orbit_regime           = 
| semimajor_axis         = 
| eccentricity           = 
| orbit_inclination      = 
| orbit_altitude         = 
| apoapsis               = 
| periapsis              = 
| orbital_period         = 
| longitude              = 
| repeat_interval        = 
| orbits_daily           = 
| repetitivity           = 
| orbit_swath            = 
| orbit_crossing         = <!-- equator crossing -->

<!-- Planetary/Lunar landing -->
| Planet                 = 
| Planet_Landing         = <!-- date/time -->
| Planet_Coords          = 
| Planet_Depart          = 
| LunarLandingDate       =
| LunarLandingCoords     =
| LunarLiftoffDate       =

<!-- Instruments -->
| Instruments            = 
| Main_Instruments       = 
| Resolution             = 
| Spectral_Band          = 
| Data_Rate              = 
| SSR                    = <!-- solid-state recorder -->
| IMG_Resolution         = 

<!-- Transponders -->
| Transponders           = 
| Transponder_Capacity   = 
| Coverage               = 
| Twta output power      = 
| Bandwidth              = 
| EIRP                   = 

| refs                   = 
| below                  = 
}}

Example from Ranger 1[çımey bıvurnê]

Ranger 1
Ranger 1
Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the Public Hall, Cleveland, Ohio, August 1964
OperatorNASA
Major contractorsJet Propulsion Laboratory
Mission typeLunar Science
Satellite ofEarth
Orbital insertion dateAugust 23, 1961 at 10:02:00 UTC
Orbits110
Launch dateAugust 23, 1961 at 06:02:00 UTC
Launch vehicleAtlas-Agena B
Launch siteCape Canaveral Missile Test Annex, Florida, United States
Mission duration7 days
Orbital decayAugust 30, 1961
COSPAR ID1961-021A
HomepageNASA NSSDC Master Catalog
Mass306.2 kg
Orbital elements
Semimajor axis6,690.3 km
Eccentricity.019939
Inclination32.9°
Apoapsis446 km
Periapsis179 km
Orbital period91.1 minutes
{{Infobox spacecraft
 | name              = Ranger 1
 | image             = [[File:Ranger 1.jpg|275px|Ranger 1]]
 | caption           = Ranger 1 Satellite in preparation for use at the Parade of Progress Show at the [[Public Auditorium|Public Hall]], [[Cleveland]], [[Ohio]], August 1964
 | organization      = [[NASA]]
 | major_contractors = [[Jet Propulsion Laboratory]]
 | mission_type      = [[Lunar Science]]
 | satellite_of      = [[Earth]]
 | orbital_insertion_date = August 23, 1961 at 10:02:00 [[Coordinated Universal Time|UTC]]
 | orbits            = 110
 | launch_date       = August 23, 1961 at 06:02:00 [[Coordinated Universal Time|UTC]]
 | launch_vehicle    = [[Atlas-Agena]] B
 | launch_site       = [[Kennedy Space Center|Cape Canaveral Missile Test Annex]], [[Florida]], [[United States]] 
 | mission_duration  = 7 days
 | decay             = August 30, 1961
 | NSSDC_ID          = 1961-021A
 | webpage           = [http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1961-021A NASA NSSDC Master Catalog]
 | mass              = 306.2 kg
 | semimajor_axis    = 6,690.3 km
 | eccentricity      = .019939
 | orbit_inclination = 32.9°
 | apoapsis          = 446 km
 | periapsis         = 179 km
 | orbital_period    = 91.1 minutes
}}

See also[çımey bıvurnê]