Launch date: December 15, 1968
Launch site: Vandenberg AFB, California
Launch vehicle: Two stage long tank 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 Earth's 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 VIII was able to transmit eight to ten images daily to nearly 400 individual ground stations around the world. ESSA VIII remained operational for 2644 days until deactivated by NASA on March 12, 1976.