Meteor-3M No.1

Last updated
Meteor-3M No.1 [1]
Meteor3M.jpg
Mission type Weather
Operator Roscosmos/Roshydromet
COSPAR ID 2001-056A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 27001
Mission durationPlanned: 3 years
In Orbit: 21 years, 9 months and 12 days
Spacecraft properties
Manufacturer VNIIEM
Launch mass2,500 kilograms (5,500 lb)
Payload mass800 kilograms (1,800 lb)
Power800 watts
Start of mission
Launch date10 December 2001, 17:18:57 (2001-12-10UTC17:18:57Z) UTC
Rocket Zenit-2
Launch site Baikonur Site 45/1
End of mission
DisposalDecommissioned
DeactivatedMarch 2006 (2006-04)
Orbital parameters
Reference system Geocentric
Regime SSO
Eccentricity 0.00135 [2]
Perigee altitude 1,016 kilometres (631 mi)
Apogee altitude 996 kilometres (619 mi)
Inclination 99.64 degrees [2]
Period 105.3 minutes [2]
 

Meteor-3M No.1 was the first and only of the Meteor-3M series polar-orbiting weather satellites. It was launched on 10 December 2001 at 17:18:57 UTC from the Baikonur Cosmodrome in Kazakhstan. [3] The satellite is in a Sun-synchronous orbit with an ascending node time of about 9AM.

Contents

Capabilities

An APT transmission was planned to only have a reduced resolution (2 km) visible channel data. The status of any APT capability on this satellite was unclear, but it was thought not to have an APT transmitter. No APT transmissions were received from this satellite. SLR mission support began on 1 May 2002.

Meteor-3M satellite atop its Zenit-2 launcher Zenit-2 rocket ready for launch.jpg
Meteor-3M satellite atop its Zenit-2 launcher

Secondary mission objective was the flight testing of the novel-type spherical retroreflector for precise laser ranging.

ILRS Mission Support Status

SLR was used for precise orbit determination and retroreflector research.

Instrumentation

Retro-reflector Array (RRA) characteristics

The retro-reflector was a glass ball 60 mm in diameter, fastened in a holder providing observation from Earth at elevations of more than 30° (the retroreflector field of view was centered in the Nadir direction). The spherical retro-reflector with its holder was fixed to the Meteor-3M No.1 spacecraft. The expected return signal strength level was between LAGEOS and ETALON.

SAGE III

Meteor-3M No.1 included the SAGE III (Stratospheric Aerosol and Gas Experiment) payload and other instruments designed to measure temperature and humidity profiles, clouds, surface properties, and high energy particles in the upper atmosphere. SAGE III was a gyrating spectrometer that measured ultraviolet/visible light, which was used to enhance understanding of natural and human-derived atmospheric processes by providing accurate long-term measurements of the vertical structure of aerosols, ozone, water vapor, and other important trace gases in the upper troposphere and stratosphere.

End of mission

Technical problems affecting the satellite two years after launch left it almost completely disabled. Meteor-3M No.1 functioned until March 2006, after which it was decommissioned. [3] Meteor-M No.1, a replacement satellite, was launched on 17 September 2009. [4]

See also

Related Research Articles

<span class="mw-page-title-main">Retroreflector</span> Device to reflect radiation back to its source

A retroreflector is a device or surface that reflects radiation back to its source with minimum scattering. This works at a wide range of angle of incidence, unlike a planar mirror, which does this only if the mirror is exactly perpendicular to the wave front, having a zero angle of incidence. Being directed, the retroflector's reflection is brighter than that of a diffuse reflector. Corner reflectors and cat's eye reflectors are the most used kinds.

<span class="mw-page-title-main">LAGEOS</span>

LAGEOS, Laser Geodynamics Satellite or Laser Geometric Environmental Observation Survey, are a series of two scientific research satellites designed to provide an orbiting laser ranging benchmark for geodynamical studies of the Earth. Each satellite is a high-density passive laser reflector in a very stable medium Earth orbit (MEO).

<span class="mw-page-title-main">Satellite laser ranging</span>

In satellite laser ranging (SLR) a global network of observation stations measures the round trip time of flight of ultrashort pulses of light to satellites equipped with retroreflectors. This provides instantaneous range measurements of millimeter level precision which can be accumulated to provide accurate measurement of orbits and a host of important scientific data. The laser pulse can also be reflected by the surface of a satellite without a retroreflector, which is used for tracking space debris.

<span class="mw-page-title-main">Project Echo</span> First passive communications satellite experiment

Project Echo was the first passive communications satellite experiment. Each of the two American spacecraft, launched in 1960 and 1964, were metalized balloon satellites acting as passive reflectors of microwave signals. Communication signals were transmitted from one location on Earth and bounced off the surface of the satellite to another Earth location.

<span class="mw-page-title-main">Meteor (satellite)</span> Series of weather observation satellites launched by Russia

The Meteor spacecraft are weather observation satellites launched by the Soviet Union and Russia. The Meteor satellite series was initially developed during the 1960s. The Meteor satellites were designed to monitor atmospheric and sea-surface temperatures, humidity, radiation, sea ice conditions, snow-cover, and clouds. Between 1964 and 1969, a total of eleven Soviet Union Meteor satellites were launched.

<span class="mw-page-title-main">ICESat</span> NASA satellite to observe ice sheets, clouds, and land; 2003–2010

ICESat was a NASA satellite mission for measuring ice sheet mass balance, cloud and aerosol heights, as well as land topography and vegetation characteristics. It operated as part of NASA's Earth Observing System (EOS). ICESat was launched 13 January 2003 on a Delta II launch vehicle from Vandenberg Air Force Base in California into a near-circular, near-polar orbit with an altitude of approximately 600 km (370 mi). It operated for seven years before being retired in February 2010, after its scientific payload shut down and scientists were unable to restart it.

<span class="mw-page-title-main">Earth Radiation Budget Satellite</span> Earth Observation Satellite (1984-2023)

The Earth Radiation Budget Satellite (ERBS) was a NASA scientific research satellite. The satellite was one of three satellites in NASA's research program, named Earth Radiation Budget Experiment (ERBE), to investigate the Earth's radiation budget. The satellite also carried an instrument that studied stratospheric aerosol and gases.

<span class="mw-page-title-main">NOAA-17</span>

NOAA-17, also known as NOAA-M before launch, was an operational, polar orbiting, weather satellite series operated by the National Environmental Satellite Service (NESS) of the National Oceanic and Atmospheric Administration (NOAA). NOAA-17 also continued the series of Advanced TIROS-N (ATN) spacecraft begun with the launch of NOAA-8 (NOAA-E) in 1983 but with additional new and improved instrumentation over the NOAA A-L series and a new launch vehicle.

The Stratospheric Aerosol and Gas Experiment (SAGE) is a series of remote sensing satellite instruments used to study the chemical composition of Earth's atmosphere. Specifically, SAGE has been used to study the Earth's ozone layer and aerosols at the troposphere through the stratosphere. The SAGE instruments use solar occultation measurement technique to determine chemical concentrations in the atmosphere. Solar occultation measurement technique measures sunlight through the atmosphere and ratios that measurement with a sunlight measurement without atmospheric attenuation. This is achieved by observing sunrises and sunsets during a satellite orbit. Physically, the SAGE instruments measure ultraviolet/visible energy and this is converted via algorithms to determine chemical concentrations. SAGE data has been used to study the atmospheres aerosols, ozone, water vapor, and other trace gases.

<span class="mw-page-title-main">NOAA-7</span>

NOAA-7, known as NOAA-C before launch, was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment. An earlier launch, NOAA-B, was scheduled to become NOAA-7, however NOAA-B failed to reach its required orbit.

NOAA-6, known as NOAA-A before launch, was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

NOAA B was an American operational weather satellite for use in the National Operational Environmental Satellite System (NOESS) and for the support of the Global Atmospheric Research Program (GARP) during 1978-1984. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

STSat-2B, or Science and Technology Satellite-2B, was a South Korean satellite which was lost in the failure of the second flight of the Naro-1 launch vehicle. It was to have been operated by the Korea Aerospace Research Institute (KARI), and was intended to demonstrate technology for future spacecraft. The satellite had a mass of 100 kg (220 lb), and was expected to operate for at least two years.

<span class="mw-page-title-main">ADEOS I</span> Japanese Earth observation satellite

ADEOS I was an Earth observation satellite launched by NASDA in 1996. The mission's Japanese name, Midori means "green". The mission ended in July 1997 after the satellite sustained structural damage to the solar panel. Its successor, ADEOS II, was launched in 2002. Like the first mission, it ended after less than a year, also following solar panel malfunctions.

<span class="mw-page-title-main">SAGE III on ISS</span>

SAGE III on ISS is the fourth generation of a series of NASA Earth-observing instruments, known as the Stratospheric Aerosol and Gas Experiment. The first SAGE III instrument was launched on a Russian Meteor-3M satellite. The recently revised SAGE III was mounted to the International Space Station where it uses the unique vantage point of ISS to make long-term measurements of ozone, aerosols, water vapor, and other gases in Earth's atmosphere.

<span class="mw-page-title-main">BLITS</span>

BLITS (Ball Lens In The Space) is a Russian satellite launched on September 17, 2009, as a secondary payload on a Soyuz-2.1b/Fregat, from the Baikonur Cosmodrome in Kazakhstan. The satellite is totally passive and spherical, and is tracked using satellite laser ranging (SLR) by the International Laser Ranging Service. The design of BLITS is based on the optical Luneburg lens concept. The retroreflector is a multilayer glass sphere; it provides uniform reflection characteristics when viewed within a very wide range of angles, and can provide a cross-section sufficient for observations at low to medium orbit heights. A similar design was already tested on a smaller laser reflector carried on board of the METEOR-3M spacecraft launched on December 10, 2001.

TanSat, also known as CarbonSat, is a Chinese Earth observation satellite dedicated to monitoring carbon dioxide in Earth's atmosphere. It is generally classified as a minisatellite, and is the first dedicated carbon mission of the Chinese space program. The mission was formally proposed in 2010, and work began in January 2011. It is funded by the Ministry of Science and Technology (MOST) and was built by the Shanghai Institute of Microsystem And Information Technology (SIMIT).

<span class="mw-page-title-main">NOAA-20</span> NASA satellite

NOAA-20, designated JPSS-1 prior to launch, is the first of the United States National Oceanic and Atmospheric Administration's latest generation of U.S. polar-orbiting, non-geosynchronous, environmental satellites called the Joint Polar Satellite System. NOAA-20 was launched on 18 November 2017 and joined the Suomi National Polar-orbiting Partnership satellite in the same orbit. NOAA-20 operates about 50 minutes behind Suomi NPP, allowing important overlap in observational coverage. Circling the Earth from pole-to-pole, it crosses the equator about 14 times daily, providing full global coverage twice a day. This gives meteorologists information on "atmospheric temperature and moisture, clouds, sea-surface temperature, ocean color, sea ice cover, volcanic ash, and fire detection" so as to enhance weather forecasting including hurricane tracking, post-hurricane recovery by detailing storm damage and mapping of power outages.

<span class="mw-page-title-main">Explorer 60</span> NASA satellite of the Explorer program

Explorer 60, also called as SAGE and was the second of the Applications Explorer Missions (AEM), AEM-B, was a NASA scientific satellite launched on 18 February 1979, from Wallops Flight Facility (WFF) by a Scout D-1 launch vehicle.

NOAA-8, known as NOAA-E before launch, was an American weather satellite operated by the National Oceanic and Atmospheric Administration (NOAA) for use in the National Environmental Satellite Data and Information Service (NESDIS). It was first of the Advanced TIROS-N series of satellites. The satellite design provided an economical and stable Sun-synchronous platform for advanced operational instruments to measure the atmosphere of Earth, its surface and cloud cover, and the near-space environment.

References

  1. "Научный Центр Оперативного Мониторинга Земли". www.ntsomz.ru. Retrieved 2016-04-03.
  2. 1 2 3 "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. Retrieved 2016-04-03.
  3. 1 2 Zak, Anatoly (4 July 2019). "Meteor spacecraft family". RussianSpaceWeb. Retrieved 24 March 2021.
  4. Clark, Stephen (17 September 2009). "Soyuz rocket launches Russian weather satellite". Spaceflight Now. Retrieved 24 March 2021.