Most Equatorial satellites are launched for commercial use (71.1%) and for the purpose of communications (57.9%).
Insights from the Equatorial satellite dataset
Which year saw the most Equatorial satellites launched?
Who operates or owns the most Equatorial satellites?
Which country operates or owns the most Equatorial satellites?
Which rocket has delivered the most Equatorial satellites to space?
Which launch site has launched the most Equatorial satellites to space?
Apogee, Perigee & Period
Highlights on some of the commercial satellites:
Second heaviest equatorial satellite launched into space at 650 kg
A commercial satellite, O3b FM09 is operated by O3b Networks Ltd. of United Kingdom for the purpose of communications.
Delivered via Soyuz-ST-B (launch vehicle) from Guiana Space Center, it was launched into space on 18 December 2014 and orbits the Earth as a equatorial MEO satellite. O3b FM09 was constructed by Thales Alenia Space (France).
O3b FM09 has a launch mass of 650 kg and navigates with the COSPAR ID 2014-083D and NORAD ID 40351.
With an orbital eccentricity of 1.73E-04, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 8,063km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 8,068km. O3b FM09 takes 288 minutes to orbit the Earth with its self-generated usable power of 1500 watts.
Heaviest satellite launched by Singapore into space at 400 kg
A commercial satellite, TeLEOS 1 is operated by AgilSpace of Singapore for the purpose of earth observation (Optical Imaging).
Constructed by ST Electronics Ltd. (Singapore), it was launched into space on 16 December 2015 using PSLV C29 as the launch vehicle from Satish Dhawan Space Centre. TeLEOS 1 orbits around the Earth as a equatorial LEO satellite.
Designated with COSPAR ID 2015-077D and NORAD ID 41169, TeLEOS 1 is designed to operate in space for a lifetime of 5 years. It has a launch mass of 400 kg.
Taking 96 minutes to orbit the Earth, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 535km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 550km. The eccentricity of the orbit is 1.08E-03 and it orbits at an inclination of 15 degrees to the equatorial plane of the Earth.
Get more insights from these satellite datasets
By Operators: SpaceX | EUTELSAT | SES | European Space Agency (ESA) | Planet Labs | Iridium | Spire Global | OneWeb | Swarm Technologies | NASA - Dataset of Satellites Launched (National Aeronautics and Space Administration) | Canadian Space Agency (CSA) - Dataset of Satellites Launched
By Launch Vehicle: Falcon 9 | Ariane 5 | Ariane 5 ECA | Delta 2 | Dnepr | Electron | Falcon Heavy | Long March 2C | Long March 2D | Long March 3B | Pegasus | Proton | Proton M | PSLV | Rokot | Soyuz | Soyuz-2.1b | Vega
By Launch Vehicle: Cape Canaveral | Baikonur Cosmodrome | Guiana Space Center | International Space Station | Jiuquan Satellite Launch Center | Plesetsk Cosmodrome | Rocket Lab Launch Complex 1 | Satish Dhawan Space Centre | Taiyuan Launch Center | Vandenberg AFB | Xichang Satellite Launch Center | Boeing Satellite Systems | Airbus Defense and Space | EADS Astrium | Lockheed Martin Commercial Space Systems | Space Systems/Loral | Surrey Satellite Technology | Technical University Berlin | Thales Alenia Space