API endpoint that allows Agencies to be viewed.

GET:
Return a list of all the existing users.

MODE:
Normal and Detailed
/2.0.0/agencies/?mode=detailed

FILTERS:
Parameters - 'featured', 'agency_type', 'country_code'
Example - /2.0.0/agencies/?featured=true

SEARCH EXAMPLE:
/2.0.0/agencies/?search=nasa

ORDERING:
Fields - 'id', 'name', 'featured'
Example - /2.0.0/agencies/?ordering=featured

GET /2.0.0/agencies/115/
HTTP 200 OK
Allow: GET
Content-Type: application/json
Vary: Accept

{
    "id": 115,
    "url": "https://ll.thespacedevs.com/2.0.0/agencies/115/",
    "name": "Arianespace",
    "featured": true,
    "type": "Commercial",
    "country_code": "FRA",
    "abbrev": "ASA",
    "description": "Arianespace SA is a multinational company founded in 1980 as the world's first commercial launch service provider. It undertakes the production, operation, and marketing of the Ariane programme. Their vehicles launch exclusively from French Guiana in South America.",
    "administrator": "CEO: Stéphane Israël",
    "founding_year": "1980",
    "launchers": "Ariane 5 | Vega",
    "spacecraft": "",
    "parent": null,
    "launch_library_url": "https://launchlibrary.net/1.4/agency/115",
    "total_launch_count": 149,
    "successful_launches": 141,
    "consecutive_successful_launches": 1,
    "failed_launches": 8,
    "pending_launches": 33,
    "successful_landings": 0,
    "failed_landings": 0,
    "attempted_landings": 0,
    "consecutive_successful_landings": 0,
    "info_url": "http://www.arianespace.com",
    "wiki_url": "http://en.wikipedia.org/wiki/Arianespace",
    "logo_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/logo/arianespace_logo_20190207032425.png",
    "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/agency_images/arianespace_image_20190207032425.jpeg",
    "nation_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/agency_nation/arianespace_nation_20190207032425.jpeg",
    "launcher_list": [
        {
            "id": 20,
            "launch_library_id": 27,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/20/",
            "name": "Ariane 5 ECA",
            "description": "Ariane 5 is a heavy-lift launch vehicle, part of the Ariane rocket family.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 ECA",
            "variant": "ECA",
            "alias": "",
            "min_stage": 0,
            "max_stage": 2,
            "length": 57.7,
            "diameter": 5.4,
            "maiden_flight": "2002-12-11",
            "launch_mass": 780,
            "leo_capacity": null,
            "gto_capacity": 10500,
            "to_thrust": 11400,
            "apogee": 40000,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252052520eca_image_20190224012333.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 8,
            "successful_launches": 71,
            "failed_launches": 2,
            "pending_launches": 7
        },
        {
            "id": 215,
            "launch_library_id": 246,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/215/",
            "name": "Ariane 5 ECA+",
            "description": "Ariane 5 ECA+ is a variant of the Ariane 5 heavy-lift vehicle, with a taller ECA-D upper stage.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 ECA+",
            "variant": "ECA+",
            "alias": "",
            "min_stage": 0,
            "max_stage": 2,
            "length": 57.7,
            "diameter": 5.4,
            "maiden_flight": "2019-08-07",
            "launch_mass": 780,
            "leo_capacity": null,
            "gto_capacity": 10200,
            "to_thrust": 11400,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane_5_eca25_image_20200220090552.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 3,
            "successful_launches": 3,
            "failed_launches": 0,
            "pending_launches": 0
        },
        {
            "id": 18,
            "launch_library_id": 9,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/18/",
            "name": "Ariane 5 ES",
            "description": "The Ariane 5 ES (Evolution Storable) has an estimated LEO launch capacity of 21,000 kg (46,000 lb). It includes all the performance improvements of Ariane 5 ECA core and boosters but replaces the ESC-A second stage with the restartable EPS used on Ariane 5 GS variants. It was used to launch the Automated Transfer Vehicle (ATV) into a 260 km circular low Earth orbit inclined at 51.6° and has been used 3 times to launch 4 Galileo navigation satellites at a time directly into their operational orbit. The Ariane 5 ES flew 8 times from 2008 to 2018 with no failures.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 ES",
            "variant": "ES",
            "alias": "",
            "min_stage": 0,
            "max_stage": 2,
            "length": 45.7,
            "diameter": 5.4,
            "maiden_flight": "2008-03-09",
            "launch_mass": 746,
            "leo_capacity": 21000,
            "gto_capacity": null,
            "to_thrust": 11400,
            "apogee": 40000,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252052520es_image_20190222031145.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 8,
            "successful_launches": 8,
            "failed_launches": 0,
            "pending_launches": 0
        },
        {
            "id": 131,
            "launch_library_id": 156,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/131/",
            "name": "Ariane 5 G",
            "description": "The original version is dubbed Ariane 5 G (Generic) and had a launch mass of 737 tonnes. Its payload capability to geostationary transfer orbit (GTO) was 6,900 kg (15,200 lb) for a single satellite or 6,100 kg (13,400 lb) for dual launches. It flew 17 times with one failure and two partial failures.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 G",
            "variant": "G",
            "alias": "",
            "min_stage": 0,
            "max_stage": 2,
            "length": 57.0,
            "diameter": 5.4,
            "maiden_flight": "1996-06-04",
            "launch_mass": 737,
            "leo_capacity": 12200,
            "gto_capacity": 6900,
            "to_thrust": null,
            "apogee": 40000,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252052520g_image_20190222030331.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 6,
            "successful_launches": 13,
            "failed_launches": 3,
            "pending_launches": 0
        },
        {
            "id": 146,
            "launch_library_id": 175,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/146/",
            "name": "Ariane 5 G+",
            "description": "The Ariane 5 G+ had an improved EPS second stage, with a GTO capacity of 7,100 kg (15,700 lb) for a single payload or 6,300 kg (13,900 lb) for two. It flew three times in 2004, with no failures.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 G+",
            "variant": "G+",
            "alias": "",
            "min_stage": 2,
            "max_stage": 2,
            "length": 55.0,
            "diameter": 5.4,
            "maiden_flight": "2004-03-02",
            "launch_mass": 750,
            "leo_capacity": null,
            "gto_capacity": 7100,
            "to_thrust": 12000,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252052520g252b_image_20190222030334.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 3,
            "successful_launches": 3,
            "failed_launches": 0,
            "pending_launches": 0
        },
        {
            "id": 149,
            "launch_library_id": 174,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/149/",
            "name": "Ariane 5 GS",
            "description": "At the time of the failure of the first Ariane 5 ECA flight in 2002, all Ariane 5 launchers in production were ECA versions. Some of the ECA cores were modified to use the original Vulcain engine and tank volumes while the failure was investigated; these vehicles were designated Ariane 5 GS. The GS used the improved EAP boosters of the ECA variant and the improved EPS of the G+ variant, but the increased mass of the modified ECA core compared to the G and G+ core resulted in slightly reduced payload capacity. Ariane 5 GS could carry a single payload of 6,600 kg (14,600 lb) or a dual payload of 5,800 kg (12,800 lb) to GTO. The Ariane 5 GS flew 6 times from 2005 to 2009 with no failures.",
            "family": "Ariane 5",
            "full_name": "Ariane 5 GS",
            "variant": "GS",
            "alias": "",
            "min_stage": 2,
            "max_stage": 2,
            "length": 55.0,
            "diameter": 5.4,
            "maiden_flight": "2005-08-11",
            "launch_mass": 750,
            "leo_capacity": null,
            "gto_capacity": 6600,
            "to_thrust": 12000,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252052520gs_image_20190222030450.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_5",
            "consecutive_successful_launches": 6,
            "successful_launches": 6,
            "failed_launches": 0,
            "pending_launches": 0
        },
        {
            "id": 121,
            "launch_library_id": 164,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/121/",
            "name": "Ariane 62",
            "description": "The Ariane 6 family is currently under development by the European Space Agency, with two variations including the Ariane 62 with two solid boosters intended for government and scientific missions.",
            "family": "Ariane",
            "full_name": "Ariane 62",
            "variant": "62",
            "alias": "",
            "min_stage": 2,
            "max_stage": 2,
            "length": 63.0,
            "diameter": 5.4,
            "maiden_flight": null,
            "launch_mass": 530,
            "leo_capacity": 10350,
            "gto_capacity": 5000,
            "to_thrust": 10370,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252062_image_20190224012339.jpeg",
            "info_url": "http://www.arianespace.com/wp-content/uploads/2017/02/Ariane6_Users-Manual_February2017.pdf",
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_6",
            "consecutive_successful_launches": 0,
            "successful_launches": 0,
            "failed_launches": 0,
            "pending_launches": 4
        },
        {
            "id": 116,
            "launch_library_id": 165,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/116/",
            "name": "Ariane 64",
            "description": "The Ariane 6 family is currently under development by the European Space Agency, with two variations including the Ariane 64 with four solid boosters intended for government and scientific missions.",
            "family": "Ariane",
            "full_name": "Ariane 64",
            "variant": "64",
            "alias": "",
            "min_stage": 2,
            "max_stage": 2,
            "length": 63.0,
            "diameter": 5.4,
            "maiden_flight": null,
            "launch_mass": 860,
            "leo_capacity": 21650,
            "gto_capacity": 11500,
            "to_thrust": 19370,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/ariane252064_image_20190603235651.jpeg",
            "info_url": "http://www.arianespace.com/wp-content/uploads/2017/02/Ariane6_Users-Manual_February2017.pdf",
            "wiki_url": "https://en.wikipedia.org/wiki/Ariane_6",
            "consecutive_successful_launches": 0,
            "successful_launches": 0,
            "failed_launches": 0,
            "pending_launches": 3
        },
        {
            "id": 49,
            "launch_library_id": 76,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/49/",
            "name": "Soyuz STA",
            "description": "The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle. This stage continues to use the RD-0110 engine.\r\n\r\nThe 2.1a/ST version is sometimes called Soyuz ST-A.",
            "family": "Soyuz",
            "full_name": "Soyuz STA/Fregat",
            "variant": "Fregat",
            "alias": "",
            "min_stage": 3,
            "max_stage": 3,
            "length": 46.3,
            "diameter": 2.95,
            "maiden_flight": "2011-12-17",
            "launch_mass": 312,
            "leo_capacity": 7020,
            "gto_capacity": 2810,
            "to_thrust": null,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/soyuz2520sta_image_20191210133244.jpg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2_(rocket)",
            "consecutive_successful_launches": 7,
            "successful_launches": 7,
            "failed_launches": 0,
            "pending_launches": 2
        },
        {
            "id": 72,
            "launch_library_id": 96,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/72/",
            "name": "Soyuz STB",
            "description": "The 2.1b version adds an upgraded engine (RD-0124) with improved performance to the second stage. First launch took place from Plesetsk Cosmodrome Site 43 on 26 July 2008 with a classified military payload.\r\n\r\nThe 2.1b/ST version is sometimes called Soyuz ST-B.",
            "family": "Soyuz",
            "full_name": "Soyuz STB Fregat-MT",
            "variant": "Fregat-MT",
            "alias": "",
            "min_stage": 3,
            "max_stage": 3,
            "length": 46.3,
            "diameter": 2.95,
            "maiden_flight": "2012-10-12",
            "launch_mass": 310,
            "leo_capacity": 8200,
            "gto_capacity": 3250,
            "to_thrust": null,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/soyuz2520stb_image_20191201201634.jpg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2#Soyuz-2.1b",
            "consecutive_successful_launches": 5,
            "successful_launches": 5,
            "failed_launches": 0,
            "pending_launches": 0
        },
        {
            "id": 171,
            "launch_library_id": 52,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/171/",
            "name": "Soyuz STB",
            "description": "The 2.1b version adds an upgraded engine (RD-0124) with improved performance to the second stage. First launch took place from Plesetsk Cosmodrome Site 43 on 26 July 2008 with a classified military payload.\r\n\r\nThe 2.1b/ST version is sometimes called Soyuz ST-B.",
            "family": "Soyuz",
            "full_name": "Soyuz STB/Fregat",
            "variant": "STB/Fregat",
            "alias": "",
            "min_stage": 3,
            "max_stage": 3,
            "length": 46.3,
            "diameter": 2.95,
            "maiden_flight": "2011-10-21",
            "launch_mass": 312,
            "leo_capacity": 8200,
            "gto_capacity": 3250,
            "to_thrust": null,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/soyuz2520stb_image_20190224025011.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Soyuz-2_(rocket)",
            "consecutive_successful_launches": 8,
            "successful_launches": 10,
            "failed_launches": 1,
            "pending_launches": 4
        },
        {
            "id": 167,
            "launch_library_id": 18,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/167/",
            "name": "Vega",
            "description": "Vega is the smallest lifter in the current Arianespace family.",
            "family": "Vega",
            "full_name": "Vega",
            "variant": "",
            "alias": "",
            "min_stage": 4,
            "max_stage": 4,
            "length": 29.9,
            "diameter": 3.025,
            "maiden_flight": "2012-02-13",
            "launch_mass": 137000,
            "leo_capacity": 1500,
            "gto_capacity": null,
            "to_thrust": 2974,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/vega_image_20201111143622.jpeg",
            "info_url": "http://www.arianespace.com/vehicle/vega/",
            "wiki_url": "https://en.wikipedia.org/wiki/Vega_(rocket)",
            "consecutive_successful_launches": 0,
            "successful_launches": 15,
            "failed_launches": 2,
            "pending_launches": 6
        },
        {
            "id": 127,
            "launch_library_id": 163,
            "url": "https://ll.thespacedevs.com/2.0.0/config/launcher/127/",
            "name": "Vega-C",
            "description": "",
            "family": "Vega",
            "full_name": "Vega-C",
            "variant": "",
            "alias": "",
            "min_stage": 1,
            "max_stage": 4,
            "length": 30.1,
            "diameter": 3.0,
            "maiden_flight": null,
            "launch_mass": 136,
            "leo_capacity": 1500,
            "gto_capacity": null,
            "to_thrust": 2974,
            "apogee": 1000,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/vega-c_image_20190224012332.jpeg",
            "info_url": "http://www.arianespace.com/vehicle/vega/",
            "wiki_url": "https://en.wikipedia.org/wiki/Vega_(rocket)",
            "consecutive_successful_launches": 0,
            "successful_launches": 0,
            "failed_launches": 0,
            "pending_launches": 7
        }
    ],
    "spacecraft_list": [
        {
            "id": 17,
            "url": "https://ll.thespacedevs.com/2.0.0/config/spacecraft/17/",
            "name": "Automated Transfer Vehicle (ATV)",
            "type": {
                "id": 1,
                "name": "Unknown"
            },
            "agency": {
                "id": 115,
                "url": "https://ll.thespacedevs.com/2.0.0/agencies/115/",
                "name": "Arianespace",
                "featured": true,
                "type": "Commercial",
                "country_code": "FRA",
                "abbrev": "ASA",
                "description": "Arianespace SA is a multinational company founded in 1980 as the world's first commercial launch service provider. It undertakes the production, operation, and marketing of the Ariane programme. Their vehicles launch exclusively from French Guiana in South America.",
                "administrator": "CEO: Stéphane Israël",
                "founding_year": "1980",
                "launchers": "Ariane 5 | Vega",
                "spacecraft": "",
                "parent": null,
                "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/agency_images/arianespace_image_20190207032425.jpeg"
            },
            "in_use": false,
            "capability": "Cargo Earth Orbit Logistics",
            "history": "During the 1990s, as the International Space Station program was taking place, it was collectively recognised by the 15 participating nations that, upon completion, the International Space Station (ISS), a crewed space station in Low Earth orbit (LEO), would require regular resupply missions in order to meet the needs of the onboard crew as well as to deliver apparatus to support the various scientific tests that would be performed on board. In October 1995, it was agreed that, amongst the various contributions to the ISS program that Europe would assume responsibility for under the vestiges of the European Space Agency (ESA), would be the Automated Transfer Vehicle, or ATV; this logistics-orientated spacecraft would perform the identified resupply missions to ISS.",
            "details": "In terms of its role, the ATV was designed to complement the smaller Russian Progress spacecraft, possessing three times its useful payload capacity. Similar to the Progress, it would carry both bulk liquids and relatively fragile freight, which would be stored within a cargo hold maintained at a pressurized shirt-sleeve environment in order that astronauts would be able to access payloads without the need to put on spacesuits. The pressurized cargo section of the ATV was based on the Italian-built Multi-Purpose Logistics Module (MPLM), which was a Shuttle-carried \"space barge\" that had been previously used for transporting equipment to and from the Station. Unlike the MPLM, the ATV used the same docking mechanism as employed upon the Progress. The ATV, like the Progress, also serves as a container for the station's waste. Each ATV weighs 20.7 tonnes at launch and has a cargo capacity of 8 tonnes.",
            "maiden_flight": "2008-03-09",
            "height": 10.3,
            "diameter": 4.5,
            "human_rated": false,
            "crew_capacity": null,
            "payload_capacity": 7667,
            "flight_life": "Six months when docked",
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/orbiter_images/automated2520transfer2520vehicle25202528atv2529_image_20190207032508.jpeg",
            "nation_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/agency_nation/automated2520transfer2520vehicle25202528atv2529_image_20190207032508.png",
            "wiki_link": "https://en.wikipedia.org/wiki/Automated_Transfer_Vehicle",
            "info_link": ""
        }
    ]
}