Şablon:Gemiya Azmini

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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
Operator NASA
Major contractors Jet Propulsion Laboratory
Mission type Lunar Science
Satellite of Earth
Orbital insertion date August 23, 1961 at 10:02:00 UTC
Orbits 110
Launch date August 23, 1961 at 06:02:00 UTC
Launch vehicle Atlas-Agena B
Launch site Cape Canaveral Missile Test Annex, Florida, United States
Mission duration 7 days
Orbital decay August 30, 1961
COSPAR ID 1961-021A
Homepage NASA NSSDC Master Catalog
Mass 306.2 kg
Orbital elements
Semimajor axis 6,690.3 km
Eccentricity .019939
Inclination 32.9°
Apoapsis 446 km
Periapsis 179 km
Orbital period 91.1 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]