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Meteor (satellite)

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Series of weather observation satellites launched by Russia This article is about satellites named "Meteor". For the process of satellites becoming meteors, see atmospheric entry and meteor.

Model of a Meteor-2 satellite

The Meteor spacecraft are weather observation satellites launched by the Soviet Union and Russia since the Cold War. 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.

Satellites

Unlike the United States, which has separate civilian and military weather satellites, the Soviet Union used a single weather satellite type for both purposes.

Meteor Prototype

Meteor Prototype launches
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 Launched as Meteor 5L
Kosmos 144 28 February 1967 1967-018A 02695 625 625 81.2° 96.9 Launched as Meteor 6L
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
References:

Meteor-1

Meteor-1 was a set of fully operational Russian meteorological satellite launched from the Plesetsk site. The satellites were placed in a near-circular, near-polar prograde orbit to provide near-global observations of the earth's weather systems, cloud cover, ice and snow fields, and reflected and emitted radiation from the dayside and nightside of the earth-atmosphere system for operational use by the Soviet Hydrometeorological Service. 31 satellites were launched between 1969 and 1981.

Meteor-1 launches
Satellite Launch date NSSDC ID SCN Apogee, km Perigee, km Inclination Period, min Note
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 Cloud Observation. End of life - 1 Dec 1976. Derelict satellite as of 3/30/2023
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 25 14 May 1976 1976-043A 08845 890 833 81.3° 102.0 meteorological satellite
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
References:

Meteor-1-25, also called "Meteor-Priroda-2", launched on 15 May 1976 by the USSR out of Plesetsk on a Vostok-2M. It was a meteorological satellite that provided global observations of the earth's weather systems, cloud cover, ice and snow fields, vertical profiles of temperature and moisture, and reflected and emitted radiation from the dayside and nightside of the earth-atmosphere system for operational use by the Soviet Hydrometeorological Service. It carried an East German-designed experimental infrared Fourier spectrometers for on-orbit testing of the new instrument for weather observation. The satellite ceased operations on three years later and is now a derelict spacecraft.

Meteor-2

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 Tsyklon-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 1,300 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. #17 broke up in June 2005.

Meteor-2-2

Meteor 2-2 launched on 6 January 1977 by the USSR out of Plesetsk on a Vostok 2-M with 1st Generation Upper Stage. It was an earth science satellite that performed cloud observation and IR temperature/humidity sounding. It ceased operations on 6 July 1978. Since then, the satellite had broken up into several pieces of debris.

Meteor-2-5

Meteor 2-5 launched on 31 October 1979 by the USSR out of Plesetsk on a Vostok 2-M with 1st Generation Upper Stage. It has undergone several breakup events, the first before January 2005 and the last as recently as 2013 or 2014, resulting in 83 known pieces of which 60 were still on-orbit as of 2019.

Meteor-2-6

Meteor 2-6 launched on 9 September 1980 by the USSR out of Plesetsk on a Vostok 2-M with 1st Generation Upper Stage. It was an Earth Science/Weather satellite that gathered meteorological information and data on penetrating radiation fluxes in circumterrestrial space. It has since broken apart into multiple pieces of space debris.

Meteor 2-7

Meteor 2-7 launched on May 14, 1981, by the USSR out of Plesetsk on a Vostok 2-M with 1st Generation Upper Stage. It had a weight of 2,750 kg, and contained the usual suite of communication and orbit control equipment powered by large solar arrays. Its mission was cloud observation and IR temperature/humidity sounding, using a Radiation Measurement Complex (RMk-2), Infrared Sounding Radiometer, Television Camera and Infrared Instrument. It ceased operations on 14 November 1982. In March 2004, it experienced an event, or a series of events, that caused it to break into 8 pieces. The cause of this break-up is unknown.

Meteor 2-8

Meteor 2-8 launched on 25 March 1982 by the USSR out of Plesetsk on a Tsyklon-3 It had a weight of 1,500 kg, and It carried scientific and meteorological instruments, and service systems. Its mission was cloud observation and IR temperature/humidity sounding, using a Radiation Measurement Complex (RMk-2), Infrared Sounding Radiometer, Television Camera and Infrared Instrument. It ceased operations on 25 September 1983. On 29 May 1999, it experienced a break-up event that caused it to break into 53 pieces. The cause of this break-up is unknown.

Meteor-2-21

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:

  1. Scanning telephotometer
  2. Scanning infrared radiometers
  3. Radiation measurement complex
  4. Retroreflector array

Meteor-Priroda

Meteor-Priroda is a series of experimental satellites launched. Internal document of Russian space agency show that it is originally only used to describe Meteor 1-31 at the time, but later extend to all experimental satellites. It is commonly perceived to only include 6 satellites: Meteor 1-18, Meteor 1-25, Meteor 1-28, Meteor 1-29, Meteor 1-30, and Meteor 1-31. Evidence suggest that Kosmos 1484 should also be included.

Meteor-Priroda series is considered to be prototypes for the Resurs O1 satellites.

Meteor-Priroda launches
This section needs expansion. You can help by adding to it. (April 2016)
Satellite Launch date NSSDC ID SCN Apogee, km Perigee, km Inclination Period, min Note
Use of Meteor-1 series platform
Meteor-Priroda 1
(Meteor-1 18)
9 July 1974 1974-052A 07363 877 905 81.2° 102.6
Meteor-Priroda 2-1
(Meteor-1 25)
15 May 1976 1976-043A 08845 866 900 81.2° 102.4
Use of Meteor-2 series platform
Meteor-Priroda 2-2
(Meteor-1 28)
29 June 1977 1977-057A 10113 602 685 98.0° 97.5
Meteor-Priroda 2-3
(Meteor-1 29)
25 January 1979 1979-005A 11251 628 657 97.9° 97.4
Meteor-Priroda 3-1
(Meteor-1 30)
18 June 1980 1980-051A 11848 589 678 97.9° 97.3
Meteor-Priroda 2-4
(Meteor-1 31)
10 July 1981 1981-065A 12585 611 688 97.9° 97.6
Meteor-Priroda 3-2
(Kosmos 1484)
24 July 1983 1983-075A 14207 595 673 98.0° 97.3
References:

Meteor-3

Launch of Meteor-3 on a Tsyklon-3 rocket

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.

Meteor-3 launches
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
References:

Meteor-3-5

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.

Meteor-3-6/PRARE

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:

  1. Scanning TV-sensor
  2. Visible light and infrared radiometers
  3. Scanning infrared radiometer
  4. Ozone Mapper
  5. Precise Range and Range-Rate Equipment (PRARE)
  6. Retroreflector array

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.

Meteor-3M

Main article: Meteor-3M No.1
Meteor-3M satellite

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.

Meteor-M

The first Meteor-M satellite, Meteor-M No.1, was launched 17 September 2009 at 16:55:07 UTC from Baikonur by a Soyuz-2-1b/Fregat rocket. Its mission ended in 2014.

The second satellite, Meteor-M No.2, was launched 8 July 2014 at 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.

Altitude of Meteor M2-2 showing the December 18th incident

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. Meteor-M No.2-3 was successfully launched on 27 June 2023, with three more satellites in various stages of development. Meteor-M No.2-4 was successfully launched on 29 February 2024 at 05:43 UTC, while Meteor-M No.2-5 is scheduled to be launched later in 2024, and No.2-6 in 2025.

Meteor-M launches
Satellite s/n Launch date NSSDC ID SCN Apogee Perigee Inclination Period
Meteor-M No.1 1 17 September 2009 2014-037A 35865 824.9 km 822.2 km 98.6° 101.2 min
Meteor-M No.2 2 8 July 2014 1985-100A 40069 833.0 km 825.9 km 98.4° 101.3 min
Meteor-M No.2-1 3 27 November 2017 Launch failure
Meteor-M No.2-2 4 5 July 2019 2019-038A 44387 819.6 km 819.3 km 98.8° 101.1 min
Meteor-M No.2-3 5 27 June 2023 2023-091A 57166 823.1 km 815.8 km 98.7° 101.1 min
Meteor-M No.2-4 5 29 February 2024 2024-039A 59051 830.4 km 819.7 km 98.6° 101.3 min

See also

  • Elektro–L, Russian geosynchronous meteorological satellites

References

  1. Soviet Weather Satellite Falls in Antarctica, RIA Novosti on SpaceDaily.com, 28 March 2012
  2. Hendrickx, Bart; Day, Dwayne A. (2 January 2024). "The Space Review: Diamonds and DORIANS: The Soviet Union's Almaz and the United States' Manned Orbiting Laboratory military space stations (part 3)". The Space Review. Retrieved 3 January 2024.
  3. ^ "Meteor-1". space.skyrocket.de. Retrieved 4 April 2016.
  4. ^ "Meteor - eoPortal Directory - Satellite Missions". directory.eoportal.org. Retrieved 5 April 2016.
  5. ^ "П. А. Румянцев. Космическая система Метеор". epizodsspace.airbase.ru. Retrieved 4 April 2016.
  6. "Meteor 1-25 - Satellite Information". Heaven's Above. Retrieved 24 January 2023.
  7. "Satellite: Meteor-P2". Retrieved 24 January 2023.
  8. "Meteor-2 (11F632)". Retrieved 26 November 2022.
  9. Gates, D.; Anz-meador, P. "An 82o Inclination Debris Cloud Revealed by Radar" (PDF). Retrieved 26 November 2022.
  10. ^ "Meteor-2". Retrieved 14 December 2022.
  11. "Satellite: Meteor 2-2". OSCAR. Retrieved 17 January 2023.
  12. "HISTORY OF ON-ORBIT SATELLITE FRAGMENTATIONS" (PDF). Retrieved 24 December 2022.
  13. "An 82o Inclination Debris Cloud Revealed by Radar" (PDF). Retrieved 24 December 2022.
  14. "Meteor 2-6". Retrieved 21 March 2023.
  15. "Launches of September 1980". Retrieved 21 March 2023.
  16. "Meteor 2-7". Retrieved 14 December 2022.
  17. "Satellite: Meteor-2-7". Retrieved 14 December 2022.
  18. Anz-Meador, Phillip D.; Opiela, John N.; Shoots, Debra (4 July 2018). HISTORY OF ON-ORBIT SATELLITE FRAGMENTATIONS (PDF). Retrieved 14 December 2022.
  19. "Meteor 2-7". Retrieved 1 January 2023.
  20. "Satellite: Meteor-2-8". Retrieved 14 December 2022.
  21. Gates, D.; Anz-Meador, P. (2019). "An 82o Inclination Debris Cloud Revealed by Radar" (PDF). First International Orbital Debris Conference. 2109: 2. Bibcode:2019LPICo2109.6038G. Retrieved 18 January 2023.
  22. Meteor-2 Archived 11 October 2011 at the Wayback Machine, Encyclopedia Astronautica, accessed 17 September 2013
  23. "Satellite Programme: Meteor-Priroda". OSCAR. Retrieved 5 December 2024.
  24. Pardini, Carmen (1 February 2005). "Survey of past on-orbit fragmentation events". Acta Astronautica. 56 (3): 379–389. doi:10.1016/j.actaastro.2004.05.065. ISSN 0094-5765.
  25. "Meteor-Priroda". space.skyrocket.de. Retrieved 5 April 2016.
  26. ^ "Meteor-3". www.astronautix.com. Archived from the original on 26 October 2010. Retrieved 19 April 2016.
  27. "Meteor-3 (17F45)". space.skyrocket.de. Retrieved 19 April 2016.
  28. "Космодром "Плесецк" | Информационный бюллетень №27". www.plesetzk.ru. Retrieved 19 April 2016.
  29. "Meteor satellite". www.russianspaceweb.com. Archived from the original on 10 April 2016. Retrieved 3 April 2016.
  30. Zak, Anatoly (15 November 2022). "The Meteor-M series". russianspaceweb.com. Retrieved 12 February 2023.
  31. Russian satellite lost after being set to launch from the wrong spaceport: Deputy prime minister admits programmers gave the US$45 million device coordinates for Baikonur rather than Vostochny cosmodrome
  32. Soyuz 2-1B launch with Meteor-M ends in apparent Fregat-M failure
  33. Zak, Anatoly (4 August 2022). "Soyuz launches fresh Meteor weather watcher and 32 small satellites". russianspaceweb.com. Retrieved 12 February 2023.
  34. "На Российском спутнике METEOR M2-2 произошла нештатная ситуация | R4UAB". r4uab.ru. Retrieved 23 December 2019.
  35. "О ситуации с КА "Метеор-М" № 2-2". roscosmos.ru. Retrieved 25 December 2019.
  36. Zak, Anatoly (27 June 2023). "Soyuz launches a Meteor weather satellite and 42 hitchhikers". RussianSpaceWeb. Retrieved 28 June 2023.
  37. "Спутник "Метеор-М" запустят на орбиту 29 февраля, сообщил источник" [The Meteor-M satellite will be launched into orbit on February 29, source says]. RIA Novosti (in Russian). 20 January 2024. Archived from the original on 21 January 2024. Retrieved 21 January 2024.
  38. "Спектрометр спутника "Метеор-МП" будет давать в два раза больше данных" [Meteor-MP satellite spectrometer will provide twice as much data]. RIA Novosti (in Russian). 19 July 2022. Retrieved 1 August 2022.

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