Launch date: November 10, 1967
Launch site: Vandenberg AFB, California
Launch vehicle: Thrust augmented Three-stage Delta
The two cameras were mounted 180 degrees opposite each other along the side of the cylindrical craft. The "cartwheel" configuration of the TIROS IX was selected as the orbital configuration of the operational series of ESSA satellites. Therefore, a camera could be pointed at some point on Earth every time the satellite rotated along its axis. The spacecraft operating system was the same as on the TIROS IX. The craft was placed in its planned sun-synchronous 101 degree inclination retrograde orbit. The satellite spin axis was rotated using the magnetic attitude control system into an alignment perpendicular to the orbital plane and tangent to the EarthÕs surface. The APT system was designed to transmit an image every 352 seconds, each photo covering a 2000 mile square area with 2 mile resolution.
ESSA VI was able to transmit up to eight images daily to individual ground stations around the world. A total of 305 receiving stations were now operational around the world, including 26 US universities, 25 US television stations, and the weather services of 45 foreign countries. ESSA VI remained operational for 465 days until deactivated by NASA on December 3, 1969.