Satellite Tracking, Prediction and Informations about

Objects in the Sky

Search Tips
You can search by Satellite Name, Norad ID or any other keyword that it is included in satellite description.

You can search for object debris if you search by word DEB and for Rocket Bodies if you search by the keyword R/B country.

Good Luck

Track Random satellites:
OPS 9431 (DSCS 2-1)

Track GOES 9 Satellite in Real Time

Detailed information about GOES 9 satellite

Designator id: 1995-025A

Description of GOES 9 Satellite:

The Geostationary Operational Environmental Satellite (GOES-J) is the second satellite in a series of next generation geosynchronous spacecraft, referred to as GOES-NEXT and represented by the GOES I through GOES M spacecraft. The GOES-NEXT series is a joint effort on the part of NASA and NOAA to provide continued operational monitoring of weather systems primarily over the United States, distribute meteorological data to regional and national weather offices within the USA, contribute to the development of an environmental data collection network, contribute to the search and rescue program, improve the capability for forcasting and provide real-time warnings of solar distrubances, and to extend knowledge and understanding of atmospheric processes to improve short and long-term weather forecasts. The GOES-NEXT series, extends the capabilities of the previous GOES 1-7 spacecraft. The GOES I-M spacecraft will be placed over the equator at 135 deg West or 75 deg West. The spacecraft structure is based on the Space Transportation System (STS)-launched, three-axis stabilized Insat (geostationary satellite for India) meteorological satellite design. The design allows unobstructed views of the Earth for operational coverage by the spacecraft sensors. The spacecraft configuration is a compact box-shaped main body that carries the Earth-observing instruments, a continuous-drive solar array attached to the south panel through a yoke assembly, and a solar pointing instrument gimbal mounted on the solar panel yoke. The main body accomodates the sensors, electronics, and support subsystems. The communication antennas, except the Tracking, Telemetry, and Command (TT&C) antenna, are hard-mounted to the Earth-facing panel. The Propulsion Module consists of the fuel and oxidizer tanks for the bipropellant propulsion subsystem mounted on the central cylinder. The Attitude and Orbit Control Substem (AOCS) provides attitude control of the spacecraft. The AOCS consists of the sensors, electronics, and the actuators. The GOES power is generated from the solar array and two 12 A-hr batteries. Power is automatically regulated during solar eclipses. The Image Navigation/Registration (INR) system provides Imager and Sounder data products in real-time to users. The Communications, Command, and Data Handling subsystem is comprised of antennas, receivers, transponders, transmitters, data encoders and encryptors and multiplexers. The Tracking Telemetry and Command (TT&C) subsystem provides the necessary monitor and command link between the spacecraft and the ground stations. The GOES-NEXT instruments consist of the following: (1) Earth Imaging System, a 5-channel visible and infrared radiometer which provides Earth imagery 24 hours a day; (2) Sounding System, a 19-channel discrete-filter radiometer for obtaining atmospheric temperature and moisture soundings; (3) a Space Environment Monitor (SEM), which consists of a magnetic field sensor, a solar X-ray sensor, an energetic particle sensor (EPS), and a High Energy Proton and Alpha Detector (HEPAD); (4) a Search and Rescue subsystem (SARSAT), which receives signals from 406 MHz distress beacons and relays them to the ground; (5) a Data Collection System (DCS) for collecting and relaying real-time information from Data Collection Platforms (DCPs) such as buoys, balloons, remote weather stations, ships, and aircraft; and (6) a Weather Facsimile (WEFAX) system which relays processed weather imagary from the Wallops Island station to the user community. The SEC package (X-rays, H+, e-, monitors, and the Magnetometer) became inoperational on or before April 2003.

Technical data:

Launch Date: 1995-05-23
Launch Vehicle: Atlas I
Launch Site: Cape Canaveral, United States
Mass: 980.0 kg
Nominal Power: 973.0 W
Funding Agencies:

NASA-Office of Space Science Applications (United States)
NOAA National Environmental Satellite Service (United States)


Earth Science
Solar Physics
Space Physics

Source: Nasa

Two Line Element Set (TLE):
1 23581U 95025A   12338.93719578 -.00000153  00000-0  10000-3 0  6537
2 23581 008.2085 055.3870 0004008 020.6005 339.3188 00.98802446 63934

Last TLE update on :2012-12-04

Find more details about GOES 9 Satellite