Agency Instance
API endpoint that allows Agencies to be viewed.
GET:
Return a list of all the existing users.
MODE:
Normal and Detailed
/2.2.0/agencies/?mode=detailed
FILTERS:
Parameters - 'featured', 'agency_type', 'country_code'
Example - /2.2.0/agencies/?featured=true
SEARCH EXAMPLE:
/2.2.0/agencies/?search=nasa
ORDERING:
Fields - 'id', 'name', 'featured'
Example - /2.2.0/agencies/?ordering=featured
The 'country_code' field is a string of comma separated ISO 3166 alpha-3 codes.
GET /2.2.0/agencies/100/?format=api
{ "id": 100, "url": "https://ll.thespacedevs.com/2.2.0/agencies/100/?format=api", "name": "Orbital Sciences Corporation", "featured": false, "type": "Commercial", "country_code": "USA", "abbrev": "OSC", "description": null, "administrator": null, "founding_year": null, "launchers": "", "spacecraft": "", "parent": null, "launch_library_url": null, "total_launch_count": 72, "successful_launches": 65, "consecutive_successful_launches": 0, "failed_launches": 7, "pending_launches": 0, "successful_landings": 0, "failed_landings": 0, "attempted_landings": 0, "consecutive_successful_landings": 0, "info_url": "http://www.orbital.com/", "wiki_url": "http://en.wikipedia.org/wiki/Orbital_Sciences_Corporation", "logo_url": null, "image_url": null, "nation_url": null, "launcher_list": [ { "id": 69, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/69/?format=api", "name": "Antares 110", "description": "Antares known during early development as Taurus II, is an expendable launch system developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems after Northrop Grumman acquired Orbital ATK) and the Yuzhnoye Design Bureau to launch the Cygnus spacecraft to the International Space Station as part of NASA's COTS and CRS programs. Able to launch payloads heavier than 5,000 kg (11,000 lb) into low-Earth orbit, Antares is the largest rocket operated by Orbital ATK. Antares launches from the Mid-Atlantic Regional Spaceport and made its inaugural flight on April 21, 2013.", "family": "Antares", "full_name": "Antares 110", "variant": "110", "alias": "", "min_stage": 1, "max_stage": 2, "length": 40.5, "diameter": 3.9, "maiden_flight": "2013-04-21", "launch_mass": 276, "leo_capacity": 4450, "gto_capacity": null, "to_thrust": 3265, "apogee": 0, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/antares_110_lau_image_20240308082903.jpg", "info_url": "http://www.northropgrumman.com/Capabilities/Antares/Pages/default.aspx", "wiki_url": "https://en.wikipedia.org/wiki/Antares_(rocket)#Antares_100", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 63, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/63/?format=api", "name": "Antares 120", "description": "Antares known during early development as Taurus II, is an expendable launch system developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems after Northrop Grumman acquired Orbital ATK) and the Yuzhnoye Design Bureau to launch the Cygnus spacecraft to the International Space Station as part of NASA's COTS and CRS programs. Able to launch payloads heavier than 5,000 kg (11,000 lb) into low-Earth orbit, Antares is the largest rocket operated by Orbital ATK. Antares launches from the Mid-Atlantic Regional Spaceport and made its inaugural flight on April 21, 2013.", "family": "Antares", "full_name": "Antares 120", "variant": "120", "alias": "", "min_stage": 2, "max_stage": 2, "length": 40.5, "diameter": 3.9, "maiden_flight": "2014-01-09", "launch_mass": 276, "leo_capacity": 4600, "gto_capacity": null, "to_thrust": 3265, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/antares_image_20190704015241.jpeg", "info_url": "http://www.northropgrumman.com/Capabilities/Antares/Pages/default.aspx", "wiki_url": "https://en.wikipedia.org/wiki/Antares_(rocket)#Antares_100", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 59, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/59/?format=api", "name": "Antares 130", "description": "Antares known during early development as Taurus II, is an expendable launch system developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems after Northrop Grumman acquired Orbital ATK) and the Yuzhnoye Design Bureau to launch the Cygnus spacecraft to the International Space Station as part of NASA's COTS and CRS programs. Able to launch payloads heavier than 5,000 kg (11,000 lb) into low-Earth orbit, Antares is the largest rocket operated by Orbital ATK. Antares launches from the Mid-Atlantic Regional Spaceport and made its inaugural flight on April 21, 2013.", "family": "Antares", "full_name": "Antares 130", "variant": "130", "alias": "", "min_stage": 2, "max_stage": 2, "length": 41.9, "diameter": 3.9, "maiden_flight": "2014-10-28", "launch_mass": 286, "leo_capacity": 5100, "gto_capacity": null, "to_thrust": 3265, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/antares_130_exp_image_20240308083257.jpg", "info_url": "http://www.northropgrumman.com/Capabilities/Antares/Pages/default.aspx", "wiki_url": "https://en.wikipedia.org/wiki/Antares_(rocket)#Antares_100", "consecutive_successful_launches": 0, "successful_launches": 0, "failed_launches": 1, "pending_launches": 0 }, { "id": 383, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/383/?format=api", "name": "Minotaur-C 1110", "description": "American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.", "family": "Minotaur-C", "full_name": "Minotaur-C 1110", "variant": "1110", "alias": "", "min_stage": 4, "max_stage": 4, "length": 27.9, "diameter": 2.35, "maiden_flight": "2000-03-12", "launch_mass": 73, "leo_capacity": 1320, "gto_capacity": null, "to_thrust": 1320, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur-C", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 384, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/384/?format=api", "name": "Minotaur-C 2110", "description": "American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.", "family": "Minotaur-C", "full_name": "Minotaur-C 2110", "variant": "2110", "alias": "", "min_stage": 4, "max_stage": 4, "length": 27.9, "diameter": 2.35, "maiden_flight": "2001-09-21", "launch_mass": 73, "leo_capacity": 1380, "gto_capacity": null, "to_thrust": 1380, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur-C", "consecutive_successful_launches": 0, "successful_launches": 1, "failed_launches": 1, "pending_launches": 0 }, { "id": 385, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/385/?format=api", "name": "Minotaur-C 2210", "description": "American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.", "family": "Minotaur-C", "full_name": "Minotaur-C 2210", "variant": "2210", "alias": "", "min_stage": 4, "max_stage": 4, "length": 29.7, "diameter": 2.35, "maiden_flight": "1998-02-10", "launch_mass": 73, "leo_capacity": 1380, "gto_capacity": null, "to_thrust": 1380, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur-C", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 386, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/386/?format=api", "name": "Minotaur-C 3110", "description": "American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.", "family": "Minotaur-C", "full_name": "Minotaur-C 3110", "variant": "3110", "alias": "", "min_stage": 4, "max_stage": 4, "length": 31.6, "diameter": 2.35, "maiden_flight": "2009-02-24", "launch_mass": 73, "leo_capacity": null, "gto_capacity": null, "to_thrust": 1380, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur-C", "consecutive_successful_launches": 0, "successful_launches": 0, "failed_launches": 1, "pending_launches": 0 }, { "id": 387, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/387/?format=api", "name": "Minotaur-C 3210", "description": "American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle, which can be launched from minimaly prepared places in a matter of a few days.", "family": "Minotaur-C", "full_name": "Minotaur-C 3210", "variant": "3210", "alias": "", "min_stage": 4, "max_stage": 4, "length": 31.6, "diameter": 2.35, "maiden_flight": "2004-05-20", "launch_mass": 73, "leo_capacity": null, "gto_capacity": null, "to_thrust": 1380, "apogee": null, "vehicle_range": null, "image_url": null, "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur-C", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 175, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/175/?format=api", "name": "Minotaur I", "description": "The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.", "family": "Minotaur", "full_name": "Minotaur I", "variant": "", "alias": "Minotaur OSP-SLV", "min_stage": 4, "max_stage": 5, "length": 19.21, "diameter": 1.67, "maiden_flight": "2000-01-27", "launch_mass": 36, "leo_capacity": 580, "gto_capacity": null, "to_thrust": 935, "apogee": null, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/minotaur2520i_image_20190224012247.jpeg", "info_url": null, "wiki_url": "http://en.wikipedia.org/wiki/Minotaur_I", "consecutive_successful_launches": 12, "successful_launches": 12, "failed_launches": 0, "pending_launches": 0 }, { "id": 108, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/108/?format=api", "name": "Minotaur IV", "description": "The Minotaur IV HAPS launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. A fourth stage, the Orion-38, is taken from the Pegasus family of air-launched rockets. A fifth stage, consisting of a hydrazine-powered motor called HAPS, increases orbital insertion accuracy and allows additional orbital maneuvering.", "family": "Minotaur", "full_name": "Minotaur IV HAPS", "variant": "HAPS", "alias": "Peacekeeper SLV", "min_stage": 5, "max_stage": 5, "length": 23.9, "diameter": 2.35, "maiden_flight": "2010-11-20", "launch_mass": 86, "leo_capacity": 1750, "gto_capacity": 0, "to_thrust": 2200, "apogee": 500, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/minotaur_iv_lau_image_20240307170209.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur_IV", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 85, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/85/?format=api", "name": "Minotaur IV", "description": "The Minotaur IV+ launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. It is similar to the Minotaur IV, but uses a larger Star-48V upper stage in place of the Orion-38 used on the baseline Minotaur IV.", "family": "Minotaur", "full_name": "Minotaur IV+", "variant": "+", "alias": "Peacekeeper SLV", "min_stage": 4, "max_stage": 4, "length": 23.9, "diameter": 2.35, "maiden_flight": "2011-09-27", "launch_mass": 86, "leo_capacity": 1950, "gto_capacity": 0, "to_thrust": 2200, "apogee": 500, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/minotaur2520iv_image_20190222030607.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur_IV", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 13, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/13/?format=api", "name": "Minotaur V", "description": "", "family": "Minotaur", "full_name": "Minotaur V", "variant": "", "alias": "", "min_stage": 1, "max_stage": 5, "length": 23.9, "diameter": 2.35, "maiden_flight": "2013-09-07", "launch_mass": 36, "leo_capacity": 1735, "gto_capacity": 0, "to_thrust": 1600, "apogee": 500, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/orbital2520atk_image_20190207032453.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Minotaur_V", "consecutive_successful_launches": 1, "successful_launches": 1, "failed_launches": 0, "pending_launches": 0 }, { "id": 119, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/119/?format=api", "name": "Pegasus", "description": "The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere.", "family": "Pegasus", "full_name": "Pegasus", "variant": "", "alias": "", "min_stage": 3, "max_stage": 3, "length": 16.9, "diameter": 1.27, "maiden_flight": "1990-04-05", "launch_mass": 18, "leo_capacity": 443, "gto_capacity": 0, "to_thrust": 580, "apogee": 4000, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/pegasus_image_20190830213841.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Pegasus_(rocket)", "consecutive_successful_launches": 4, "successful_launches": 4, "failed_launches": 0, "pending_launches": 0 }, { "id": 132, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/132/?format=api", "name": "Pegasus HAPS", "description": "The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere.\r\nThe HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.", "family": "Pegasus", "full_name": "Pegasus HAPS", "variant": "HAPS", "alias": "", "min_stage": 0, "max_stage": 5, "length": 15.5, "diameter": 1.28, "maiden_flight": "1991-07-17", "launch_mass": 18, "leo_capacity": 250, "gto_capacity": 0, "to_thrust": 580, "apogee": 4000, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/pegasus_image_20190830213841.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Pegasus_(rocket)", "consecutive_successful_launches": 2, "successful_launches": 2, "failed_launches": 0, "pending_launches": 0 }, { "id": 129, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/129/?format=api", "name": "Pegasus Hybrid", "description": "The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere.", "family": "Pegasus", "full_name": "Pegasus Hybrid", "variant": "Hybrid", "alias": "", "min_stage": 0, "max_stage": 3, "length": 15.5, "diameter": 1.28, "maiden_flight": "1995-04-03", "launch_mass": 18, "leo_capacity": 350, "gto_capacity": 0, "to_thrust": 580, "apogee": 4000, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/pegasus_image_20190830213841.jpg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Pegasus_(rocket)", "consecutive_successful_launches": 4, "successful_launches": 4, "failed_launches": 0, "pending_launches": 0 }, { "id": 173, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/173/?format=api", "name": "Pegasus XL", "description": "The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere.", "family": "Pegasus", "full_name": "Pegasus XL", "variant": "", "alias": "", "min_stage": 0, "max_stage": 3, "length": 17.6, "diameter": 1.27, "maiden_flight": "1994-06-27", "launch_mass": 23, "leo_capacity": 443, "gto_capacity": 0, "to_thrust": 580, "apogee": 4000, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/pegasus_xl_moun_image_20240307124328.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Pegasus_(rocket)", "consecutive_successful_launches": 25, "successful_launches": 28, "failed_launches": 3, "pending_launches": 0 }, { "id": 118, "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/118/?format=api", "name": "Pegasus XL HAPS", "description": "The Pegasus is an air-launched rocket developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems). Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, the vehicle consists of three solid propellant stages and an optional monopropellant fourth stage. Pegasus is released from its carrier aircraft at approximately 40,000 ft (12,000 m), and its first stage has a wing and a tail to provide lift and attitude control while in the atmosphere.\r\nThe HAPS variant adds a Hydrazine Auxiliary Propulsion System maneuvering stage.", "family": "Pegasus", "full_name": "Pegasus XL HAPS", "variant": "HAPS", "alias": "", "min_stage": 0, "max_stage": 4, "length": 17.6, "diameter": 1.27, "maiden_flight": "1997-12-23", "launch_mass": 23, "leo_capacity": 443, "gto_capacity": 0, "to_thrust": 580, "apogee": 4000, "vehicle_range": null, "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/pegasus_xl_moun_image_20240307124328.jpeg", "info_url": null, "wiki_url": "https://en.wikipedia.org/wiki/Pegasus_(rocket)", "consecutive_successful_launches": 5, "successful_launches": 5, "failed_launches": 0, "pending_launches": 0 } ], "spacecraft_list": [] }
