| ESSA-9 | |
| Mission Type: | Meteorology |
| Operator: | ESSA (1969-70) NOAA (1970-72) |
| Cospar Id: | 1969-016A |
| Satcat: | 3764 |
| Mission Duration: | 1,726 days (achieved) (in orbit) |
| Launch Mass: | 145kg (320lb) |
| Instruments: | Advanced Vidicon Camera System (AVCS), Flat Plate Radiometer (FPR)[1] |
| Launch Date: | UTC[2] |
| Launch Rocket: | Delta E1 |
| Launch Site: | Cape Canaveral LC-17B |
| Disposal Type: | Decommissioned |
| Orbit Epoch: | December 7, 2013, 20:28:49 UTC[3] |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Low Earth |
| Orbit Periapsis: | 1432km (890miles) |
| Orbit Apoapsis: | 1512km (940miles) |
| Orbit Semimajor: | 7843.18km (4,873.53miles) |
| Orbit Inclination: | 101.99 degrees |
| Orbit Eccentricity: | 0.00508 |
| Orbit Mean Motion: | 12.49 |
| Orbit Period: | 115.21 minutes |
| Apsis: | gee |
| Programme: | TOS |
| Previous Mission: | ESSA-8 |
| Next Mission: | TIROS-M |
ESSA-9, also known as TOS-G, was a meteorological satellite.[4] Its name was derived from that of its oversight agency, the Environmental Science Services Administration (ESSA). ESSA-9 replaced the ESSA-7 satellite.
ESSA-9 was launched on a three-stage Delta rocket from Cape Canaveral, Florida. The launch occurred at 07:47 UTC (02:47 EDT) on February 26, 1969. The spacecraft was placed in a Sun-synchronous orbit of 101.4° inclination. Immediately after launch ESSA-9 had a perigee of 1427km (887miles) and an apogee of 1508km (937miles), giving it an orbital period of 115.2 minutes, or a mean motion of 12.5 orbits per day.[2] ESSA-9 operated for 1,726 days before it was deactivated in November 1972.
The ESSA-9 spacecraft was similar to the TIROS series of satellites, having an 18-sided polygonal shape that measured 42inches in diameter and 22inches high. It weighed 320lb. The body of ESSA-9 was made of aluminum alloy and stainless steel. The shell of the craft was covered with 10,020 solar cells.[5] The solar cells recharged the 63 nickel–cadmium batteries during the time the spacecraft was in sunlight. ESSA-9 employed the same cartwheel-style stabilization as the TIROS-9 satellite. The satellite used a magnetic attitude spin coil (MASC) to control its attitude while in orbit. The magnetic field induced by the MASC's current interacted with the Earth's magnetic field to provide the torque necessary to maintain a desired spin rate of 9.225 rpm.[6]
ESSA-9 carried two sets of two main instruments, the Advanced Vidicon Camera System (AVCS) and the Flat Plate Radiometer (FPR). The AVCS was used to collect imagery of cloud cover on Earth. The cameras had a resolution of 2miles and covered an area of 2000sqmi. The cameras took single images of a particular region of the Earth's surface once a day. The FPR's were used to measure the global distribution of solar radiation reflected by the Earth and the Earth's atmosphere. They also measured long-wave emissions from the Earth. The sensors used in the ESSA satellites were from the earlier Nimbus program.