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/37/?format=api
HTTP 200 OK
Allow: GET
Content-Type: application/json
Vary: Accept

{
    "id": 37,
    "url": "https://ll.thespacedevs.com/2.2.0/agencies/37/?format=api",
    "name": "Japan Aerospace Exploration Agency",
    "featured": true,
    "type": "Government",
    "country_code": "JPN",
    "abbrev": "JAXA",
    "description": "The Japan Aerospace Exploration Agency (JAXA) is Japan's national aero-space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and the launch of satellites into orbit, and is involved in many more advanced missions, such as asteroid exploration and possible manned exploration of the Moon. JAXA launch their Epsilon vehicle from the Uchinoura Space Center and their H-II vehicles from the Tanegashima Space Center.",
    "administrator": "Administrator: Hiroshi Yamakawa",
    "founding_year": "2003",
    "launchers": "H-II",
    "spacecraft": "",
    "parent": null,
    "launch_library_url": null,
    "total_launch_count": 36,
    "successful_launches": 32,
    "consecutive_successful_launches": 1,
    "failed_launches": 4,
    "pending_launches": 4,
    "successful_landings": 0,
    "failed_landings": 0,
    "attempted_landings": 0,
    "consecutive_successful_landings": 0,
    "info_url": "http://www.jaxa.jp/",
    "wiki_url": "http://en.wikipedia.org/wiki/Japan_Aerospace_Exploration_Agency",
    "logo_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/japan2520aerospace2520exploration2520agency_logo_20190207032440.png",
    "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/japan2520aerospace2520exploration2520agency_image_20190207032440.jpeg",
    "nation_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/japan2520aerospace2520exploration2520agency_nation_20230531052930.png",
    "launcher_list": [
        {
            "id": 112,
            "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/112/?format=api",
            "name": "Epsilon",
            "description": "The Epsilon rocket is a Japanese solid-fuel rocket designed to launch scientific satellites. It is a follow-on project to the larger and more expensive M-V rocket which was retired in 2006. The Japan Aerospace Exploration Agency (JAXA) began developing the Epsilon in 2007. It is capable of placing a 590 kg payload into Sun-synchronous orbit.",
            "family": "Epsilon",
            "full_name": "Epsilon",
            "variant": "",
            "alias": "",
            "min_stage": 3,
            "max_stage": 4,
            "length": 24.4,
            "diameter": 2.5,
            "maiden_flight": "2013-09-14",
            "launch_mass": 91,
            "leo_capacity": null,
            "gto_capacity": null,
            "to_thrust": 2271,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/epsilon_image_20221009075145.jpg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Epsilon_(rocket)",
            "consecutive_successful_launches": 0,
            "successful_launches": 5,
            "failed_launches": 1,
            "pending_launches": 0
        },
        {
            "id": 115,
            "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/115/?format=api",
            "name": "Epsilon S",
            "description": "The Epsilon S rocket is a Japanese solid-fuel rocket designed to launch scientific satellites. It is a follow-on project to the larger and more expensive M-V rocket which was retired in 2006. The Japan Aerospace Exploration Agency (JAXA) began developing the Epsilon in 2007. The first stage is based on SRB-3, the strap-on solid-rocket booster of H3",
            "family": "Epsilon",
            "full_name": "Epsilon S",
            "variant": "S",
            "alias": "",
            "min_stage": 4,
            "max_stage": 4,
            "length": 24.4,
            "diameter": 2.5,
            "maiden_flight": "2013-09-14",
            "launch_mass": 91,
            "leo_capacity": null,
            "gto_capacity": null,
            "to_thrust": 2158,
            "apogee": null,
            "vehicle_range": null,
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/epsilon_image_20190207032600.jpeg",
            "info_url": null,
            "wiki_url": "https://en.wikipedia.org/wiki/Epsilon_(rocket)#Epsilon_S",
            "consecutive_successful_launches": 0,
            "successful_launches": 0,
            "failed_launches": 0,
            "pending_launches": 3
        },
        {
            "id": 122,
            "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/122/?format=api",
            "name": "SS-520",
            "description": "The fourth configuration of SS-520. It would have been the smallest and lightest vehicle to put something into orbit, but it lost telemetry and was told to abort, falling into the ocean.",
            "family": "S-Series",
            "full_name": "SS-520-4",
            "variant": "4",
            "alias": "",
            "min_stage": 3,
            "max_stage": 3,
            "length": 9.7,
            "diameter": 0.5,
            "maiden_flight": "2017-01-14",
            "launch_mass": 3,
            "leo_capacity": 4,
            "gto_capacity": null,
            "to_thrust": null,
            "apogee": 1000,
            "vehicle_range": null,
            "image_url": null,
            "info_url": null,
            "wiki_url": "https://ja.wikipedia.org/wiki/SS-520%E3%83%AD%E3%82%B1%E3%83%83%E3%83%88",
            "consecutive_successful_launches": 0,
            "successful_launches": 0,
            "failed_launches": 1,
            "pending_launches": 0
        },
        {
            "id": 144,
            "url": "https://ll.thespacedevs.com/2.2.0/config/launcher/144/?format=api",
            "name": "SS-520",
            "description": "The fifth configuration of the SS-520, succeeded as the smallest rocket to put something into orbit. It holds this title to this day.",
            "family": "S-Series",
            "full_name": "SS-520-5",
            "variant": "5",
            "alias": "",
            "min_stage": 3,
            "max_stage": 3,
            "length": null,
            "diameter": 0.5,
            "maiden_flight": "2018-02-03",
            "launch_mass": 3,
            "leo_capacity": 4,
            "gto_capacity": null,
            "to_thrust": null,
            "apogee": 1000,
            "vehicle_range": null,
            "image_url": null,
            "info_url": null,
            "wiki_url": "https://ja.wikipedia.org/wiki/SS-520%E3%83%AD%E3%82%B1%E3%83%83%E3%83%88",
            "consecutive_successful_launches": 1,
            "successful_launches": 1,
            "failed_launches": 0,
            "pending_launches": 0
        }
    ],
    "spacecraft_list": [
        {
            "id": 18,
            "url": "https://ll.thespacedevs.com/2.2.0/config/spacecraft/18/?format=api",
            "name": "H-II Transfer Vehicle (HTV)",
            "type": {
                "id": 4,
                "name": "Cargo Resupply"
            },
            "agency": {
                "id": 37,
                "url": "https://ll.thespacedevs.com/2.2.0/agencies/37/?format=api",
                "name": "Japan Aerospace Exploration Agency",
                "featured": true,
                "type": "Government",
                "country_code": "JPN",
                "abbrev": "JAXA",
                "description": "The Japan Aerospace Exploration Agency (JAXA) is Japan's national aero-space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and the launch of satellites into orbit, and is involved in many more advanced missions, such as asteroid exploration and possible manned exploration of the Moon. JAXA launch their Epsilon vehicle from the Uchinoura Space Center and their H-II vehicles from the Tanegashima Space Center.",
                "administrator": "Administrator: Hiroshi Yamakawa",
                "founding_year": "2003",
                "launchers": "H-II",
                "spacecraft": "",
                "parent": null,
                "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/japan2520aerospace2520exploration2520agency_image_20190207032440.jpeg",
                "logo_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/logo/japan2520aerospace2520exploration2520agency_logo_20190207032440.png"
            },
            "in_use": false,
            "capability": "Cargo Earth Orbit Logistics",
            "history": "Like the European Automated Transfer Vehicle the Japan Aerospace Exploration Agency had agreed to take part in the resupply operations of the international space station and developed the HTV to perform this task.",
            "details": "The HTV is about 9.8 metres (32 ft) long (including maneuvering thrusters at one end) and 4.4 metres (14 ft) in diameter. Total mass when empty is 10.5 tonnes (11.6 short tons), with a maximum total payload of 6,000 kilograms (13,000 lb; 6.0 t; 6.6 short tons), for a maximum launch weight of 16.5 tonnes (18.2 short tons). The HTV is comparable in function to the Russian Progress, European ATV, commercial Dragon, and commercial Cygnus spacecraft, all of which bring supplies to the ISS. Like the ATV, the HTV carries more than twice the payload of the Progress, but is launched less than half as often. Unlike Progress capsules and ATVs, which use the docking ports automatically, HTVs and American commercial spacecraft approach the ISS in stages, and once they reach their closest parking orbit to the ISS, crew grapple them using the robotic arm Canadarm2 and berth them to an open berthing port on the Harmony module.",
            "maiden_flight": "2009-09-10",
            "height": 9.8,
            "diameter": 4.4,
            "human_rated": false,
            "crew_capacity": null,
            "payload_capacity": 6000,
            "payload_return_capacity": 20,
            "flight_life": "Solo flight about 100 hours, stand-by more than a week, docked with the ISS about 30 days.",
            "image_url": "https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/images/htv-4_captured__image_20240325122159.jpeg",
            "nation_url": null,
            "wiki_link": "https://en.wikipedia.org/wiki/H-II_Transfer_Vehicle",
            "info_link": ""
        }
    ]
}