Organization | DigitalGlobe |
---|---|
NSSDC ID | 2001-047A |
SATCAT | 26953 |
Mission Type | Earth observation |
Contractor | Ball Aerospace & Technologies[1] |
Satellite of | Earth |
Launch date | October 18, 2001, 18:51 UTC |
Rocket | Delta 7320-10 D288 |
Launch site | |
Design life | 5 years[2] |
Mission duration | 13 years and 2 months |
Launch mass | 1,100 kg (2,400 lb)[2] |
Dry mass | 951 kg (2,097 lb) |
Decay date | January 27, 2015 |
Webpage | Official website |
Orbital elements | |
Semi-major axis | 6,828 kilometers (4,243 mi) |
Perigee | 460 kilometers (290 mi) |
Apogee | 464 kilometers (288 mi) |
Inclination | 97.2 degrees |
Eccentricity | 0.00029 |
Orbital period | 93.8 minutes |
Instruments | |
Visible cameras | 61 cm panchromatic 2.4 meter multispectral |
QuickBird was a high-resolution commercial earth observation satellite, owned by DigitalGlobe launched in 2001 and [3] decayed in 2015.[4] It was the first satellite in a constellation of three scheduled to be in orbit by 2008. QuickBird used Ball Aerospace's Global Imaging System 2000 (BGIS 2000).[1] The satellite collected panchromatic (black and white) imagery at 61 centimeter resolution and multispectral imagery at 2.44- (at 450 km) to 1.63-meter (at 300 km) resolution, as orbit altitude is lowered during the end of mission life.[5]
At this resolution, detail such as buildings and other infrastructure are easily visible. However, this resolution is insufficient for working with smaller objects such as a license plate on a car. The imagery can be imported into remote sensing image processing software, as well as into GIS packages for analysis.
Contractors include Ball Aerospace & Technologies, Kodak and Fokker Space.
WorldView-3 is the industry’s first multi-payload, super-spectral, high-resolution commercial satellite. Operating at an altitude of 617 km, WorldView-3 provides 31 cm panchromatic resolution, 1.24 m multispectral resolution, 3.7 m short-wave infrared resolution, and 30 m CAVIS resolution. ° Super-spectral imagery ° Large area mono. DigitalGlobe is the global leader in satellite imagery, geospatial information, and location-based intelligence.
QuickBird I[edit]
The first QuickBird was launched in November 2000, by EarthWatch from the Plesetsk Cosmodrome in Russia. QB-1 failed to reach planned orbit and was declared a failure.[6] Prior to QuickBird I and II, DigitalGlobe launched the EarlyBird 1 successfully in 1997 but the satellite lost communications after only four days in orbit due to power system failure.[2]
QuickBird II[edit]
QuickBird II (also QuickBird-2 or Quickbird 2), was launched October 18, 2001 from the Vandenberg Air Force Base, California, aboard a Boeing Delta II rocket.[2] The satellite was initially expected to collect at 1 meter resolution but after a license was granted in 2000 by the U.S. Department of Commerce / NASA, DigitalGlobe was able launch the QuickBird II with 0.61 meter panchromatic and 2.4 meter multispectral (previously planned 4 meter) resolution.[2]
Mission Extension[edit]
In April 2011, the Quickbird satellite was raised from an orbit of 450 km (280 mi) to 482 km (300 mi).[7] The process, started in March 2011, extended the satellite's life. Before the operation the useful life of Quickbird was expected to drop off around mid-2012 but after the successful mission, the new orbit prolonged the satellite life into early 2015.
Decaying[edit]
The last picture was acquired on December 17, 2014. On January 27, 2015 QuickBird re-entered Earth’s atmosphere.
Specifications[edit]
Sensors
- 60 cm (24 in) (1.37 μrad) panchromatic at nadir
- 2.4 m (7 ft 10 in) (5.47 μrad) multispectral at nadir
- MS Channels: blue (450-520 nm), green (520-600 nm), red (630-690 nm), near-IR (760-890 nm)[8]
Swath width and area size
- Nominal swath width: 18 km at nadir
- Accessible ground swath: 544 km centered on the satellite ground track (to 30° off nadir)
- Area of interest
- Single area: 18 km by 18 km
- Strip: 18 km by 360 km
Orbit
- Altitude (original): 450 km – 97.2 degree sun synchronous circular orbit[2]
- Altitude (post-orbit modification): 482 km – 98 degree sun synchronous inclination
- Revisit frequency: 1 to 3.5 days depending on latitude at 60 cm resolution[8]
- Viewing angle: Agile spacecraft, in-track and cross-track pointing[8]
- Period 94.2 minutes
On-board storage
- 128 Gigabit capacity (approximately 57 single area images)
Spacecraft
- Fueled for 7 years
- 2100 lb (950 kg), 3.04 m (10 ft) in length
Launch[edit]
- Launch Date: October 18, 2001[2]
- Launch Window: 1851-1906 GMT (1451-1506 EDT)
- Launch Vehicle: Delta II
- Launch Site: SLC-2W, Vandenberg Air Force Base, California
- USAF Designation: Quickbird 2.[9]
See also[edit]
References[edit]
- ^ abBall Aerospace: QuickBird
- ^ abcdefg'QuickBird-2'. EOPortal.org. Retrieved June 11, 2014.
- ^[1]
- ^Digitalglobe: QuickBirdArchived May 17, 2008, at the Wayback Machine
- ^'DigitalGlobe Data Sheet: Quickbird'(PDF). DigitalGlobe.com. DigitalGlobe. February 12, 2014. Retrieved June 19, 2014.
- ^DigitalGlode History - QuickBird IArchived September 23, 2009, at the Wayback Machine
- ^'DigitalGlobe Completes Quickbird Satellite Orbit Raise'. DigitalGlobe News Room. April 18, 2011. Archived from the original on July 14, 2014. Retrieved June 11, 2014.
- ^ abc'QuickBird 2 was successfully launched on 18 Oct 2001'. Center for Remote Imaging, Sensing & Processing. 2001. Retrieved June 11, 2014.
- ^Mehuron, Tamar A., Assoc. Editor (August 2008). '2008 USAF Space Almanac - Major Civilian Satellites in Military Use'(PDF). Air Force Magazine. Vol. 91 no. 8. Pub: Air Force Association. pp. 49–50.CS1 maint: Extra text: authors list (link)
External links[edit]
- DigitalGlobe - QuickBird specifications