Model of the Ørsted Satellite in the Tycho Brahe Planetarium
|Mission type||Earth observation|
|Operator||Danish Meteorological Institute|
|Mission duration||15 years, 10 months, 9 days|
|Manufacturer||Computer Resources International|
|Launch mass||61 kg (134 lb)|
|Dry mass||50 kg (110 lb)|
|Dimensions||34x45x72 cm (and an 8 m boom)|
|Power||54.0 W (nominal)|
|Start of mission|
|Launch date||23 February 1999, 10:29:55UTC|
|Rocket||Delta II 7920-10 D267|
|Launch site||Vandenberg SLC-2W|
|Semi-major axis||7,111.179 km (4,418.682 mi)|
|Perigee||632.6 km (393.1 mi)|
|Apogee||833.4 km (517.9 mi)|
|Argument of perigee||10.0389 degrees|
|Mean anomaly||29.8678 degrees|
|Epoch||14 December 2013, 14:18:37 UTC|
Ørsted is Denmark's first satellite, named after Hans Christian Ørsted (1777–1851) a Danish physicist and professor at the University of Copenhagen. It is in an almost sun synchronous low Earth orbit.
After more than ten years in orbit, the Ørsted satellite is still operational, and continues to downlink accurate measurements of the Earth's magnetic field. Ørsted was constructed by a team of Danish space companies, of which CRI was prime contractor. CRI was acquired by Terma A/S before Ørsted was launched, and the daily operations are being run as a teamwork between Terma A/S and the Danish Meteorological Institute.
The main scientific objective of the spacecraft was to map the Earth's magnetic field and collect data to determine the changes occurring in the field.
Based on data from the Ørsted satellite, researchers from Danish Space Research Institute concluded that the Earth's magnetic poles are moving, and that the speed with which they are moving has been increasing for the past few years. This apparent acceleration indicates, that the poles of the Earth might be in the process of switching around, which could have serious consequences for land-based biological life.
The primary scientific instruments on the Ørsted satellite are:
- Overhauser magnetometer provides extremely accurate measurements of the strength of the magnetic field. The Overhauser magnetometer is situated at the end of an 8 meter long boom, in order to minimize disturbances from the satellite's electrical systems.
- CSC fluxgate vector magnetometer, used to measure the strength and direction of the magnetic field. The CSC magnetometer is situated somewhat closer to the satellite body in the so-called "gondola", together with the
- Star Imager, used to determine the orientation of both the satellite and the CSC magnetometer.
The other three instruments are located in the main body of the satellite:
- Charged Particle Detector, used to measure the flux of fast electrons, protons and alpha particles around the satellite.
- BlackJack GPS Receiver, developed by the NASA Jet Propulsion Laboratory and used to accurately determine the satellite's position; can also be used to monitor the atmospheric pressure, temperature and humidity profile on the path between Ørsted and GPS satellites through atmospheric occultation.
- Trimble TANS GPS Receiver, also used to determine the satellite's position as a backup to the BlackJack.
- Purucker, M., Langlais, B., Olsen, N., Hulot, G. & Mandea, M.: The southern edge of cratonic North America: Evidence from new satellite magnetometer observations, Geophys.Res.Lett., 29(15), 8000, doi:10.1029/2001GL013645, 2002 [part of a special issue on results from the Ørsted satellite. Plate 3 from this paper is the cover of a special Ørsted issue on August 1, 2002 (Issue #15).]
- Hulot, G., Eymin, C., Langlais, B., Mandea, M. & Olsen, N.: Small-scale structure of the geodynamo inferred from Oersted and Magsat satellite data, Nature, Volume 416, Issue 6881, pp. 620-623 (April 2002)
- Neubert, T., Mandea, M., Hulot, G., von Frese, R., Primdahl, F., Jørgensen, J.L., Friis-Christensen, E., Stauning, P., Olsen, N. & Risbo, T.: Ørsted Satellite Captures High-Precision Geomagnetic Field Data, EOS, Vol. 82, No. 7, p. 81, 87, and 88, Feb. 13, 2001
- Montenbruck, O; Garcia-Fernandez, M; Williams, J (2006). "Performance comparison of semicodeless GPS receivers for LEO satellites". GPS Solutions (Springer-Verlag) 10 (4): 249–261. doi:10.1007/s10291-006-0025-9. Retrieved 2014-04-15.