1. Remote Sensing and Active Tectonics Barry Parsons and Richard Walker Michaelmas Term 2013 Lecture 2

2. Satellite Orbits (1) 1.Satellite orbit is an ellipse, with the centre of mass of the Earth at one focus of the ellipse. 2.In practice, remote sensing satellites are in almost circular orbits, i.e. the eccentricity e is small (e << 1).

3. Newton’s law of motion: Newton’s law of gravitation: Period of orbit: Altitude (km)Period 20088 mins 70099 mins 360001447 mins = 24.11 hours M F R v m Satellite Orbits (2)

4. Athens Istanbul

5. What was the Time of Day? Mount Parnassos Delphi

6. Effect of Time of Day on the Image 1.Time of day affects length of shadow. It is this contrast that reveals reveals topographic features. Want some shadowing, i.e. not midday when Sun is overhead, but not too much, i.e. not early morning. Time of day also affects illumination. 2.If the orbital plane remained fixed in space, which is what would happen if the earth really did act like a point mass, then the time the image was acquired would vary throughout the year as the Earth rotates about the Sun. 3.It is convenient if the images at a given location are always acquired at the same solar time.

7. Orbital Precession 1.The satellite moving round its orbit has angular momentum like a top. 2.The mass in the equatorial bulge produces a net torque on the satellite. 3.The torque causes the orbital plane to precess like the earth’s gravity causes a top to precess.

8. Sun-synchronous Orbits Rate of orbital precession: For sun-synchronous orbits: km (J 2 is the coefficient of the P 2 0 term in the expansion for the gravitational potential that describes the gravitational effect of the equatorial bulge.)

9. Choosing the Orbital Parameters 1.The period of orbital motion is determined by the orbital radius R and inclination i. 2.For any R can choose i such that orbit is sun-synchronous. 3.Also choose R and i such that the period of orbital motion satisfies the condition where Ω e is the rate of rotation of the Earth, and n o and n r are integers. This condition means that, after n o orbits and n r rotations of the Earth relative to the orbital plane, the orbit retraces its ground track. This means that any location can be re-imaged on a regular basis. For Landsat 7 coverage repeats after 233 orbits and 16 days.

10. Orbital Parameters for Landsat 7

11. Ground Coverage for Landsat 7

12. Imaging by Line Scanning

13. Spectral Bands For Landsat 7 Enhanced Thematic Mapper

14. Line Scanning System for Landsat 7

15. Arrangement of Detectors for Landsat 7 ETM

16. Location of 1999 Izmit Earthquake

17. Landsat TM image (542) acquired 1 day after the 1999 Izmit earthquake Landsat Image Scanning Revealed by Saturated Band

18. SPOT Earth Observation Satellites Dual InstrumentsPushbroom Recording

19. Band Spectral Range (μm) Resolution (m) (Spot 1-3) Resolution (m) (Spot 4) Resolution (m) (Spot 5) 10.50-0.5920 10 20.61-0.6820 10 30.79-0.8920 10 SWIR1.58-1.7520 Panchromatic0.51-0.7310 Panchromatic0.61-0.6810 Panchromatic0.49-0.692.5/5 Spectral Bands for Spot Satellites

20. SpotLandsat Altitude822 km705 km Inclination98°98.2° Period101.4 mins98.8 mins W track drift2823 km2752 km Revs/day14+5/2614+9/16 Cycle duration26 days16 days Orbits per cycle369233 Swath width60 km185 km Stereo Imaging by the Spot Satellites