The Coriolis satellite is a Naval Research Laboratory (NRL) and Air Force Research Laboratory (AFRL) Earth and space observation satellite launched from Vandenberg Air Force Base, on 2003-01-06 at 14:19 GMT.
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Mission type | Earth and Solar observation |
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Operator | NRL, AFRL |
COSPAR ID | 2003-001A ![]() |
SATCAT no. | 27640![]() |
Spacecraft properties | |
Manufacturer | Spectrum Astro Inc |
Launch mass | 395 kilograms (871 lb) |
Power | 1,174 watts |
Start of mission | |
Launch date | January 6, 2003, 14:19 (2003-01-06UTC14:19Z) UTC |
Rocket | Titan II(23)G |
Launch site | Vandenberg SLC-4W |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.0013721 |
Perigee altitude | 826 kilometers (513 mi) |
Apogee altitude | 846 kilometers (526 mi) |
Inclination | 98.7 degrees |
Period | 101.5 minutes |
Epoch | 14 November 2016, 20:52:53 UTC |
Instruments | |
WindSat, SMEI | |
WINDSAT is a joint Integrated Program Office/Department of Defense demonstration project, intended to measure ocean surface wind speed and wind direction from space using a polarimetric radiometer. WINDSAT was developed and managed by the Space Test Program at Kirtland AFB in New Mexico, designed for a three-year lifetime. It is primarily designed to measure ocean surface wind direction (nonprecipitating conditions) with a 25-km spatial resolution. Secondary measurements are Sea surface temperature, soil moisture, rain rate, ice and snow characteristics and water vapor.
The Solar Mass Ejection Imager (SMEI) is an instrument intended to detect disturbances in the solar wind by means of imaging scattered light from the free electrons in the plasma of the solar wind. To do this three CCD cameras observe sections of the sky of size 60 by 3 degree.
As the SMEI instrument observes the whole sky, data generated has been used to observe periodic changes in the brightness of stars. This data can be used to detect asteroseismological oscillation in giant stars, and for the detection of large eclipsing extra-solar planets.
U.S. Air Force Research Laboratory (AFRL) spacecraft and air vehicles | |
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Launch/orbital vehicles |
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University Nanosat Program | |
Space weather satellites | |
Technology demonstrators |
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Tactical Satellite Program satellites |
← 2002 · Orbital launches in 2003 · 2004 → | |
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Coriolis | ICESat · CHIPSat | STS-107 (SpaceHab RDM · EDO) | SORCE | USA-166 · XSS-10 | Progress M-47 | Intelsat 907 | USA-167 | IGS-1A · IGS-1B | USA-168 | Molniya-1 No.92 | USA-169 | INSAT-3A · Galaxy 12 | AsiaSat-4 | Kosmos 2397 | Soyuz TMA-2 | GALEX | GSAT-2 | Hayabusa (Minerva) | Hellas Sat 2 | Beidou 1C | Mars Express (Beagle 2) | Kosmos 2398 | AMC-9 | Progress M1-10 | Thuraya 2 | Spirit | Optus and Defence C1 · BSAT-2c | Molniya-3 No.53 | Orbview-3 | Monitor-E GVM · MIMOSA · DTUSat · MOST · Cute-I · QuakeSat · AAU-Cubesat · CanX-1 · Cubesat XI-IV | Opportunity | Rainbow 1 | EchoStar IX | Kosmos 2399 | SCISAT-1 | Kosmos 2400 · Kosmos 2401 | Spitzer | Progress M-48 | USA-170 | USA-171 | PS-2 | Mozhaets-4 · NigeriaSat-1 · UK-DMC · BILSAT-1 · Larets · STSAT-1 · Rubin-4 | e-Bird · INSAT-3E · SMART-1 | Galaxy 13/Horizons-1 | Shenzhou 5 | Resourcesat-1 | Soyuz TMA-3 | USA-172 | CBERS-2 · Chuang Xin 1 | SERVIS-1 | FSW-18 | Shen Tong 1 | Yamal-201 · Yamal-202 | IGS-2A · IGS-2B | USA-173 | Gruzomaket | Kosmos 2402 · Kosmos 2403 · Kosmos 2404 | USA-174 | USA-175 | Amos-2 | Ekspress AM22 | Tan Ce 1 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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