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Envisat

ESA Earth observation satellite (2002–2012)

Envisat

ESA Earth observation satellite (2002–2012)

FieldValue
nameEnvisat
imageEnvisatmod.jpg
image_captionModel of Envisat
mission_typeEarth observation
operatorESA
website
COSPAR_ID2002-009A
SATCAT27386
mission_durationPlanned: 5 years
Final:
manufacturerAstrium
launch_mass8211 kg
dimensions26 xx
power6,500 watts
instruments
launch_dateUTC
launch_rocketAriane 5G V-145
launch_siteKourou ELA-3
launch_contractorArianespace
last_contact
(spacecraft failure)
declared
disposal_typeNone
decay_date~150 years
orbit_epoch15 December 2013, 03:07:00 UTC
orbit_referenceGeocentric
orbit_regimePolar low Earth
orbit_semimajor7144.9 km
orbit_periapsis772 km
orbit_apoapsis774 km
orbit_inclination98.40 degrees
orbit_repeat35 days
orbit_period100.16 minutes
orbit_eccentricity0.00042
apsisgee

Final: (spacecraft failure)

Envisat ("Environmental Satellite") is a large Earth-observing satellite which has been inactive since 2012. It was launched on 1 March 2002 aboard an Ariane 5 from the Guyana Space Centre in Kourou, French Guiana, into a Sun synchronous polar orbit at an altitude of 790 ± 10 km.

Operated by the European Space Agency (ESA), it was the world's largest civilian Earth observation satellite. Its objective was to support the continuity of European Remote-Sensing Satellite missions, providing additional observations to improve environmental studies. To accomplish the global and regional objectives of the mission, numerous scientific disciplines used the data acquired from the sensors on the satellite to study atmospheric chemistry, ozone depletion, biological oceanography, ocean temperature and colour, wind waves, hydrology (humidity, floods), agriculture and arboriculture, natural hazards, digital elevation modelling (using interferometry), monitoring of maritime traffic, atmospheric dispersion modelling (pollution), cartography and snow and ice.

Envisat malfunctioned before it could be deorbited, and after losing contact with the satellite on 8 April 2012, ESA formally announced the end of Envisat's mission on 9 May 2012. The defunct satellite is considered space debris and orbits the Earth in about 101 minutes, with a repeat cycle of 35 days. An analysis that determined the 50 "statistically most concerning" debris objects in low Earth orbit ranked Envisat in 21st place.

Envisat was able to operate five years beyond its planned mission lifetime, delivering over a petabyte of data. At the time of its failure, Envisat had cost a total of 2.5 billion euro to develop, launch, and operate. The mission has been replaced by the Sentinel series of satellites. The first of these, Sentinel 1, has taken over the radar duties of Envisat since its launch in 2014.

Mission

Envisat was launched as an Earth observation satellite. Its objective was to support the continuity of European Remote-Sensing Satellite missions, providing additional observations to improve environmental studies.

To accomplish the global and regional objectives of the mission, numerous scientific disciplines used the data acquired from the sensors on the satellite to study atmospheric chemistry, ozone depletion, biological oceanography, ocean temperature and colour, wind waves, hydrology (humidity, floods), agriculture and arboriculture, natural hazards, digital elevation modelling (using interferometry), monitoring of maritime traffic, atmospheric dispersion modelling (pollution), cartography and snow and ice.

Specifications

;Dimensions 26 m × 10 m × 5 m in orbit with the solar array deployed.

;Mass 8211 kg, including 319 kg of fuel and a 2118 kg instrument payload. ;Power Solar array with a total load of 3560 W.

Instruments

find=Envisat instruments}}

Envisat carries an array of nine Earth-observation instruments that gathered information about the Earth (land, water, ice, and atmosphere) using a variety of measurement principles. A tenth instrument, DORIS, provided guidance and control. Several of the instruments were advanced versions of instruments that were flown on the earlier ERS-1 and ERS 2 missions and other satellites.

MWR

MWR (Microwave Radiometer) was designed for measuring water vapour in the atmosphere.

AATSR

Main article: AATSR

AATSR (Advanced Along Track Scanning Radiometer) can measure the sea surface temperature in the visible and infrared spectra. It is the successor of ATSR1 and ATSR2, payloads of ERS 1 and ERS 2. AATSR can measure Earth's surface temperature to a precision of 0.3 K-change, for climate research. Among the secondary objectives of AATSR is the observation of environmental parameters such as water content, biomass, and vegetal health and growth.

MIPAS

MIPAS (Michelson Interferometer for Passive Atmospheric Sounding) is a Fourier transforming infrared spectrometer which provides pressure and temperature profiles, and profiles of trace gases nitrogen dioxide (), nitrous oxide (), methane (), nitric acid (), ozone (), and water () in the stratosphere. The instrument functions with high spectral resolution in an extended spectral band, which allows coverage across the Earth in all seasons and at equal quality night and day. MIPAS has a vertical resolution of 3 to depending on altitude (the larger at the level of the upper stratosphere).

MERIS

Main article: MERIS

MERIS (MEdium Resolution Imaging Spectrometer) measures the reflectance of the Earth (surface and atmosphere) in the solar spectral range (390 to 1040 nm) and transmits 15 spectral bands back to the ground segment. MERIS was built at the Cannes Mandelieu Space Center.

SCIAMACHY

Main article: SCIAMACHY

SCIAMACHY (SCanning Imaging Absorption spectroMeter for Atmospheric CHartographY) compares light coming from the sun to light reflected by the Earth, which provides information on the atmosphere through which the Earth-reflected light has passed.

SCIAMACHY is an image spectrometer with the principal objective of mapping the concentration of trace gases and aerosols in the troposphere and stratosphere. Rays of sunlight that are reflected transmitted, backscattered and reflected by the atmosphere are captured at a high spectral resolution (0.2 to 0.5 nm) for wavelengths between 240 and 1700 nm, and in certain spectra between 2,000 and 2,400 nm. Its high spectral resolution over a wide range of wavelengths can detect many trace gases even in tiny concentrations. The wavelengths captured also allow effective detection of aerosols and clouds. SCIAMACHY uses 3 different targeting modes: to the nadir (against the sun), to the limbus (through the atmospheric corona), and during solar or lunar eclipses. SCIAMACHY was built by Netherlands and Germany at TNO/TPD, SRON and Airbus Defence and Space Netherlands.

RA-2

RA-2 (Radar Altimeter 2) is a dual-frequency Nadir pointing Radar operating in the Ku band and S bands, it is used to define ocean topography, map/monitor sea ice and measure land heights.

Mean sea level measurements from Envisat are continuously graphed at the Centre National d'Etudes Spatiales web site, on the Aviso page.

ASAR

ASAR (Advanced Synthetic Aperture Radar) operates in the C band in a wide variety of modes. It can detect changes in surface heights with sub-millimeter precision. It served as a data link for ERS 1 and ERS 2, providing numerous functions such as observations of different polarities of light or combining different polarities, angles of incidence and spatial resolutions.

ModeIdPolarisationIncidenceResolutionSwath
Alternating polarisationAPHH/VV, HH/HV, VV/VH15–45°30–150 m58–110 km
ImageIMHH, VV15–45°30–150 m58–110 km
WaveWVHH, VV400 m5 km × 5 km
Suivi global (ScanSAR)GMHH, VV1000 m405 km
Wide Swath (ScanSAR)WSHH, VV150 m405 km

These different types of raw data can be given several levels of treatment (suffixed to the ID of the acquisition mode: IMP, APS, and so on):

  • RAW (raw data, or "Level 0"), which contains all the information necessary to create images.
  • S (complex data, "Single Look Complex"), images in complex numeric form, the real and imaginary parts of the output of the compression algorithm
  • P (precision image), amplified image with constant pixel width (12.5 m for IMP)
  • M (medium precision image), amplified radiometry image with a resolution greater than P
  • G (geocoded image), amplified image to which simple geographical transforms have been applied to show relief.

Data capture in WV mode is unusual in that they constitute a series of 5 km × 5 km spaced at 100 km.

DORIS

Main article: DORIS (geodesy)

DORIS (Doppler Orbitography and Radiopositioning Integrated by Satellite) determines the satellite's orbit to within 10 cm.

GOMOS

Main article: GOMOS

GOMOS (Global Ozone Monitoring by Occultation of Stars) looks at stars as they descend through the Earth's atmosphere and change colour, allowing measurement of gases such as ozone (), including their vertical distribution.

GOMOS uses the principle of occultation. Its sensors detect light from a star traversing the Earth's atmosphere and measures the depletion of that light by trace gases nitrogen dioxide (), nitrogen trioxide, (), ), ozone () and aerosols present between about 20 to altitude. It has a resolution of 3 km.

End of mission

Loss of contact

ESA announced on 12 April 2012 that they lost contact with Envisat on Sunday, 8 April 2012, after 10 years of service, exceeding the initially planned life span by 5 years. The spacecraft was still in a stable orbit, but attempts to contact it were unsuccessful. Ground-based radar and the French Pleiades Earth probe were used to image the silent Envisat and look for damage. ESA formally announced the end of Envisat's mission on 9 May 2012.

Envisat was launched in 2002 and it operated five years beyond its planned mission lifetime, delivering over a petabyte of data. ESA was planning to operate the spacecraft until 2014.

Space safety

The defunct Envisat satellite is considered space debris and orbits the Earth in about 101 minutes, with a repeat cycle of 35 days. It poses a hazard because of the risk of collisions. Given its orbit and its area-to-mass ratio, it will take about 150 years for the satellite to be gradually pulled into the Earth's atmosphere. Envisat is currently orbiting in an environment where two catalogued space debris objects can be expected to pass within about 200 m of it every year, which would likely trigger the need for a manoeuvre to avoid a possible collision. A collision between a satellite the size of Envisat and an object as small as 10 kg could produce a very large cloud of debris, initiating a self-sustaining chain-reaction of collisions and fragmentation with production of new debris, a phenomenon known as the Kessler Syndrome.

Envisat was a candidate for a mission to remove it from orbit, called e.Deorbit. The spacecraft sent to bring down Envisat would itself need to have a mass of approximately 1.6 tonnes.

References

References

  1. (15 December 2013). "ENVISAT Satellite details 2002-009A NORAD 27386". N2YO.
  2. [https://earth.esa.int/web/guest/missions/esa-operational-eo-missions/envisat EarthNet Online]
  3. (9 May 2012). "ESA declares end of mission for Envisat". ESA.
  4. "EnviSat (Environmental Satellite)".
  5. [https://earth.esa.int/web/guest/missions/esa-operational-eo-missions/envisat/satellite/space-segment Envisat – Overall configuration]
  6. "I - Sciamachy".
  7. "Breaking News {{pipe}} Flagship Envisat satellite stops communicating". Spaceflight Now.
  8. "ESA Portal – Envisat services interrupted". Esa.int.
  9. [http://www.space.com/15369-mysteriously-silent-envisat-satellite-space-photos.html Huge, Mysteriously Silent Satellite Spotted by Another Spacecraft] Space.com article, 20 April 2012
  10. [https://www.bbc.co.uk/news/science-environment-17692027 Contact lost with flagship Envisat spacecraft] 12 April 2012.
  11. [http://spacenews.com/envisat-pose-big-orbital-debris-threat-150-years-experts-say/ "Envisat To Pose Big Orbital Debris Threat for 150 Years, Experts Say."] ''SpaceNews''. Retrieved: 27 September 2015.
  12. Gini, Andrea. (25 April 2012). "Don Kessler on Envisat and the Kessler Syndrome". Space Safety Magazine.
  13. (13 October 2020). "Upper stages top list of most dangerous space debris".
  14. (6 May 2014). "e.Deorbit Symposium". ESA.
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