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[clarification needed] were designed to monitor atmospheric and sea-surface temperatures, humidity, radiation, sea ice conditions, snow-cover, and clouds.[not verified in body] Between 1964 and 1969 a total of eleven Soviet Union Meteor satellites were launched.
Meteor 1-26 was considered to be the most likely candidate for a 7 January 2017 satellite near collision. The Joint Space Operations Center which announced the possible collision didn't identify the satellites involved but third-party observers were of the opinion that Meteor 1-26 and DMSP F15 were the most likely candidates.
|Satellite||Launch date||NSSDC ID||SCN||Apogee, km||Perigee, km||Inclination||Period, min||Note|
|Kosmos 44||28 August 1964||1964-053A||00876||857||615||65.04°||Technology demonstrator|
|Kosmos 58||26 February 1965||1965-014A||01907||647||563||65°||Technology demonstrator|
|Kosmos 100||17 December 1965||1965-106A||01843||658||630||65°||Technology demonstrator|
|Kosmos 118||11 May 1966||1966-038A||02168||657||587||65°||Technology demonstrator|
|Kosmos 122||25 June 1966||1966-057A||02254||683||657||65.14°||97.12||Technology demonstrator|
|Kosmos 144||28 February 1967||1967-018A||02695||625||625||81.2°||96.9|
|Kosmos 156||27 April 1967||1967-039A||02762||630||630||81.2°||97.0|
|Kosmos 184||24 October 1967||1967-102A||03010||635||635||81.2°||97.1|
|Kosmos 206||14 March 1968||1968-019A||03150||630||630||81.2°||97.0|
|Kosmos 226||12 June 1968||1968-049A||03282||603||650||81.2°||96.9|
|—||1 February 1969||—||—||—||—||—||—||Launch failure|
|Meteor-1 1||26 March 1969||1969-029A||03835||644||713||81.2°||97.9|
|Meteor-1 2||6 October 1969||1969-084A||04119||630||690||81.2°||97.7|
|Meteor-1 3||17 March 1970||1970-019A||04349||555||643||81.2°||96.4|
|Meteor-1 4||28 April 1970||1970-037A||04393||637||736||81.2°||98.1|
|Meteor-1 5||23 June 1970||1970-047A||04419||863||906||81.2°||102.0|
|Meteor-1 6||15 October 1970||1970-085A||04583||633||674||81.2°||97.5|
|Meteor-1 7||20 January 1971||1971-003A||04849||630||767||81.2°||97.6|
|Meteor-1 8||17 April 1971||1971-031A||05142||620||646||81.2°||97.2|
|Meteor-1 9||16 July 1971||1971-059A||05327||618||650||81.2°||97.3|
|Meteor-1 10||29 December 1971||1971-120A||05731||880||905||81.2°||102.7|
|Meteor-1 11||30 March 1972||1972-022A||05917||878||903||81.2°||102.6|
|Meteor-1 12||30 June 1972||1972-049A||06079||897||929||81.2°||103.0|
|Meteor-1 13||27 October 1972||1972-085A||06256||893||904||81.2°||102.6|
|Meteor-1 14||20 March 1973||1972-085A||06392||882||903||81.2°||102.6|
|Meteor-1 15||29 May 1973||1973-034A||06659||867||909||81.2°||102.5|
|Meteor-1 16||5 March 1974||1974-011A||07209||853||906||81.2°||102.2|
|Meteor-1 17||24 April 1974||1974-025A||07274||877||907||81.2°||102.6|
|Meteor-1 19||28 October 1974||1974-083A||07490||855||917||81.2°||102.5|
|Meteor-1 20||17 December 1974||1974-099A||07574||861||910||81.2°||102.4|
|Meteor-1 21||1 April 1975||1975-023A||07714||877||906||81.2°||102.6|
|Meteor-1 22||18 September 1975||1975-087A||08293||867||918||81.2°||102.3|
|Meteor-1 23||25 December 1975||1975-124A||08519||857||913||81.2°||102.4|
|Meteor-1 24||7 April 1976||1976-032A||08799||863||906||81.2°||102.3|
|Meteor-1 26||16 October 1976||1976-102A||09481||871||904||81.3°||102.5|
|Meteor-1 27||5 April 1977||1977-024A||09903||869||909||81.3°||102.5|
The Meteor-2 series, based on the Meteor-1, was the second generation of Soviet meteorological satellites. They were launched into orbit at first by the Vostok-2M launch vehicle until that was replaced by the Tsiklon-3 launch vehicle in the early 1980s. Between 1975 and 1993, 21 Meteor-2's were launched. They were flown in non-sun-synchronous polar orbits with altitudes between 850 and 950 km and inclinations of 81-82º. They weighed about 1300 kg and had two solar arrays.
The instruments consisted of three television-type (frame technique) VIS and IR scanners, a five-channel scanning radiometer and a radiometer (RMK-2) for measuring radiation flux densities in the near-Earth space.
In addition to its regular payload, Meteor-2 21 carried a unique Fizeau Retro Reflector Array (RRA) for Satellite Laser Ranging applications.
Several of the satellites have begun to break up and create debris. #16 broke up in 1998 after a propulsion failure. #18 broke up the following year for unknown reasons. #4 broke up in March 2004. #5 is believed to have started to break up prior to 2005. #17 broke up in June 2005.
Meteor-2-21/Fizeau is the twenty-first and last in the Meteor-2 series of Russian meteorological satellites.
ILRS Mission Support Status: Satellite Laser Ranging (SLR) tracking support of this satellite was discontinued in October 1998. What makes Meteor-2-21 distinctive from the other meteorological satellites is its unique retroreflector array. The name Fizeau is derived from a French physicist, Armand Fizeau who, in 1851, conducted an experiment which tested for the aether convection coefficient. SLR tracking of this satellite was used for precise orbit determination and the Fizeau experiment. The Fizeau experiment tests the theory of special relativity – that distance events that are simultaneous for one observer will not be simultaneous for another observer who is in motion relative to the first observer.
Retroreflector Array (RRA) Characteristics: The retro-reflector array consists of three corner cubes in a linear array with the two outer corner cubes pointing at 45 degree angles relative to the central cube. The central cube is made of fused silica and has a two-lobe Far Field Diffraction Pattern (FFDP) providing nearly equal intensities for compensated and uncompensated velocity aberration. Both outer reflectors have aluminum coating on the reflecting surfaces and near-diffraction-limited FFDPs. One of the end reflectors is made of fused silica with an index of refraction of 1.46 and should provide partial compensation of the velocity aberration. The other end reflector is made of fused glass with an index of refraction of 1.62 and should provide a perfect compensation of the velocity aberration.
SLR full-rate data from MOBLAS 4, MOBLAS 7, and Maidanak seem to confirm the presence of the compensating influence of the Fizeau effect. Resur-1, another Russian satellite launched in 1994, has 2 corner cubes reflectors with near diffraction-limited FFDPs, which were specifically designed for the continuation of this experiment. WESTPAC, a future SLR satellite, will verify indisputably the existence or otherwise of the Fizeau effect.
Instrumentation: Meteor-2-21/Fizeau had the following instrumentation on board:
|Satellite||Launch date||NSSDC ID||SCN||Apogee, km||Perigee, km||Inclination||Period, min||Note|
|Use of Meteor-1 series platform|
|9 July 1974||1974-052A||07363||877||905||81.2°||102.6|
|15 May 1976||1976-043A||08845||866||900||81.2°||102.4|
|Use of Meteor-2 series platform|
|29 June 1977||1977-057A||10113||602||685||98.0°||97.5|
|25 January 1979||1979-005A||11251||628||657||97.9°||97.4|
|18 June 1980||1980-051A||11848||589||678||97.9°||97.3|
|10 July 1981||1981-065A||12585||611||688||97.9°||97.6|
The Meteor-3 series was launched 7 times between 1984 and 1994 after a difficult and protracted development program that began in 1972. All the satellites were launched on Tsyklon-3 rockets. These satellites provide weather information including data on clouds, ice and snow cover, atmospheric radiation and humidity. The Meteor-3 class of satellites orbit in a higher altitude than the Meteor-2 class of satellites thus providing more complete coverage of the Earth's surface. The Meteor-3 has the same payload as the Meteor-2 but also includes an advanced scanning radiometer with better spectral and spatial resolution and a spectrometer for determining total ozone content. Meteorological data is transmitted to four primary sites in the former Soviet Union in conjunction with about 80 other smaller sites.
|Satellite||s/n||Launch date||NSSDC ID||SCN||Apogee, km||Perigee, km||Inclination||Period, min||Note|
|Kosmos 1612||1||27 November 1984||1984-120A||15406||130.2||1230.8||82.61°||98.15||launch failure, stage 3 failed to reignite|
|Meteor-3 1||2||24 October 1985||1985-100A||16191||1236.0||1264.0||82.53°||110.32|
|Meteor-3 2||3||26 July 1988||1988-064A||19336||1198.2||1221.9||82.55°||109.42|
|Meteor-3 3||4||25 October 1989||1989-086A||20305||1191.0||1228.0||82.57°||109.49|
|Meteor-3 4||6||24 April 1991||1991-030A||21232||1190.0||1229.0||82.55°||109.50|
|Meteor-3 5||5||15 August 1991||1991-056A||21655||1199.7||1220.1||82.57°||109.40|
|Meteor-3 6||7||25 January 1994||1994-003A||22969||1191||1228||82°||109.40|
Meteor-3-5, launched in 1991, is in a slightly higher orbit than Meteor-2-21, and operated until 1994. It transmitted on 137.300 MHz. Mechanically, it is similar to Meteor-2-21. Which satellite was in operation depended on the sun angles and consequently the seasons. Meteor-3-5 was usually the (Northern Hemisphere) "summer" satellite while 2-21 was in operation for approximately the half-year centered on winter. The satellite carried the second Total Ozone Mapping Spectrometer (TOMS) aloft as the first and the last American-built instrument to fly on a Soviet spacecraft. Launched from the Plesetsk, Russia, facility near the White Sea, on 15 August 1991, Meteor-3 TOMS had a unique orbit that presents special problems for processing data. Meteor-3 TOMS began returning data in August 1991 and stopped in December 1994.
The Meteor-3-6/PRARE satellite is the sixth in the Russian Meteor-3 series of meteorological satellites launched in 1994.
ILRS Mission Support Status: Satellite laser ranging and PRARE data was used for precision orbit determination and intercomparison of the two techniques. ILRS tracking support of this satellite was discontinued on 11 November 1995.
Instrumentation: Meteor-3-6 has the following instrumentation on board:
RetroReflector Array (RRA) Characteristics: The retro-reflector array is a box wing annulus with a diameter of 28 cm and has 24 corner cube reflectors.
Main article: Meteor-3M No.1
The Meteor-3M series of satellites was to be an advanced series of polar orbiters with one 1.4 km resolution visible channel and a ten-channel radiometer with 3 km resolution. Initially four Meteor-3M satellites were planned, however due to financial difficulties only one was launched.
The first Meteor-M satellite, Meteor-M No.1, was launched 17 September 2009 16:55:07 UTC from Baikonur by a Soyuz-2-1b/Fregat rocket. Its mission ended in 2014.[full citation needed]
The second satellite, Meteor-M No.2, was launched 8 July 2014 16:58:28 UTC from Baikonur by a Soyuz-2-1b/Fregat rocket. Its mission is scheduled to last 5 years.
On 27 November 2017, the launch of Meteor-M No.2-1 was lost after a programming error; also lost were 18 smaller satellites from other nations.
On 5 July 2019, the replacement satellite for the failed Meteor-M No.2-1 satellite, the Meteor-M No.2-2 (also known as Meteor M2-2) was launched from Vostochny cosmodrome.[full citation needed][needs update]
On 18 December 2019, image downlink from Meteor-M No.2-2 ceased. Tracking revealed the craft had suffered degradation in orbit with a 2 km (1.2 mi) decrease in perigee. NORAD was not able to identify any space object involved in a collision. Roscosmos later confirmed that the satellite had suffered a decompression of its thermal control system following what is presumed to be a micrometeoroid impact. Following the incident, the spacecraft was automatically switched into a low-power mode and ground operators worked to restore the satellite's orbit and orientation. By 25 December 2019, the satellite had resumed controlled flight, but the future of its mission remains uncertain.
More Meteor-M satellites are currently being developed. As of August 2022, Meteor-M No.2-3 and No.2-4 are scheduled for launch in 2023, No.2-5 in 2024, and No.2-6 in 2025.