Lockheed Martin Commercial Space Systems - Constructed Satellites Dataset
This dataset contains 29 entries.

  Overview

This is a dataset of satellites constructed by Lockheed Martin Commercial Space Systems, based on UCS Satellite Database compiled by the Union of Concerned Scientist (UCS).


  Data Table

Preparing data

  More..

Insights from the dataset of satellites constructed by Lockheed Martin Commercial Space Systems

  Which year saw the most satellites launched?

The years are 2006 and 2000, which saw the launch of 4 satellites constructed by Lockheed Martin Commercial Space Systems.

  Who operates or owns the most satellites constructed by Lockheed Martin Commercial Space Systems?

SES S.A. owns/operates the most number of satellites constructed by Lockheed Martin Commercial Space Systems (12 - 41.4% of the satellites in this dataset).

  Which country operates or owns the most satellites constructed by Lockheed Martin Commercial Space Systems?

Japan and USA own/operate the most number of satellites constructed by Lockheed Martin Commercial Space Systems (9 - 31.0% of the satellites in this dataset).

  Which rocket has delivered the most satellites constructed by Lockheed Martin Commercial Space Systems to space?

The rocket that has delivered the most satellites constructed by Lockheed Martin Commercial Space Systems to space is Ariane 5 ECA which has delivered 7 satellites (24.1%).

  Which launch site has launched the most satellites constructed by Lockheed Martin Commercial Space Systems to space?

The launch site that has delivered the most satellites constructed by Lockheed Martin Commercial Space Systems to space is Guiana Space Center which has launched 18 satellites (62.1%).

  Apogee, Perigee & Period

The perigees (point of the orbit closest to the Earth's center of mass) of the satellites range from 33,066km to 35,784km, with the average perigee being 35,681.2km from the Earth, while the apogees (point of the orbit farthest from the Earth's center of mass) of the satellites range from 35,725km to 35,810km, with the average apogee being 35,793.3km from the Earth. The longest period a satellite takes to orbit around the Earth is 1,436 minutes.

  Satellite Mass

The launch masses (include fuel) of the satellites range from 1,980kg to 5,857kg, while the dry masses (excluding fuel) of the satellites range from 860kg to 2,600kg.


Highlights on some of the satellites constructed by Lockheed Martin Commercial Space Systems:

JCSat 17.

JCSAT-17 and GEO-KOMPSAT-2B satellites separation

  Heaviest satellite launched by Japan into space at 5,857 kg

Operated by Sky Perfect JSAT Corporation of Japan, JCSat 17 is a commercial satellite launched for the purpose of communications.

Constructed by Lockheed Martin Commercial Space Systems (USA), it was launched into space on 18 February 2020 using Ariane 5 as the launch vehicle from Guiana Space Center. JCSat 17 orbits around the Earth as a GEO satellite.

JCSat 17 has a launch mass of 5,857 kg and is expected to have a operational lifetime of 15 years. It navigates with the COSPAR ID 2020-013A and NORAD ID 45245.

With an orbital eccentricity of 3.20E-04, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 35,773km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 35,800km. It takes 1,436 minutes to orbit the Earth.

JCSat 17 orbits along the longitude of 136 degrees at an inclination of 7 degrees.

 

 Compare JCSat 17 with USA 202 from USA.

 Compare JCSat 17 with TIBA-1 from Egypt.


Intelsat 901.

MEV-1 and IS-901 Mission Profile | Intelsat

  Second heaviest satellite launched by Atlas 2AS into space at 4,723 kg

A commercial satellite, Intelsat 901 is operated by Intelsat S.A. of USA for the purpose of communications.

Constructed by Lockheed Martin Commercial Space Systems (USA), it was launched into space using Atlas 2AS as the launch vehicle from Cape Canaveral on 9 June 2001. Intelsat 901 orbits around the Earth as a GEO satellite.

With a launch mass of 4,723kg and a dry mass of 1,972kg, Intelsat 901 is designed to operate in space for a lifetime of 13 years. It orbits around the Earth with the COSPAR ID 2001-024A and NORAD ID 26824.

With an orbital eccentricity of 2.73E-04, the satellite's perigee, which is the point of the orbit closest to the Earth's center of mass, is 35,775km while its apogee, which is the point of the orbit farthest from the Earth's center of mass, is 35,798km. It takes 1,436 minutes to orbit the Earth.

With generated usable power of 10000 watts, Intelsat 901 orbits along the longitude of -28 degrees.

 

 Compare Intelsat 901 with Echostar 16 from USA.

 Compare Intelsat 901 with AMC-18 from USA.


Get more insights from these satellite datasets

  Full datasets:  All satellites by launch date   |   The Heaviest Satellites That Are Launched to Space

  By Use Type:  Civil-use satellites   |   Commercial satellites   |   Government satellites   |   Military satellites

  By Country:  USA   |   UK   |   France   |   Germany   |   Japan   |   China   |   Russia   |   Australia   |   Canada

  By Orbit Class/Type:  LEO satellites   |   MEO satellites   |   GEO satellites   |   Elliptical orbit   |   Polar orbit   |   Equatorial orbit   |   Non-polar inclined orbit   |   Sun-synchronous orbit   |   Molniya orbit

  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


  Interactive Chart

Chart 1: Major Operators
Preparing chart
Chart 2: Satellites by Purpose
Preparing chart
Chart 3: Satellites by Country
Preparing chart

  Attributions

No attribution sources specified.
...

Disclaimer :Please be advised that RList does not endorse nor guarantee the completeness, accuracy, reliability or validity of any information published by our member curators herein. For more details, please refer to our Website Terms of Use.