@prefix skos: . @prefix ns0: . skos:prefLabel "Earth Observation Satellites"@en ; a skos:Concept ; skos:narrower . ns0:altLabel [ ] ; skos:definition """The Earth Probe TOMS (EP-TOMS) spacecraft was launched on July 2, 1996 from a Pegasus XL rocket and placed into a polar orbit with the following characteristics: Apogee Altitude : 515.2 km Perigee Altitude : 490.5 km Orbit Inclination : 97.432 deg. Period : 94.6 min The satellite was built by TRW for NASA's Goddard Space Flight Center. TOMS is part of NASA's Mission to Planet Earth a long term, coordinated research effort to study the Earth as a global environmental system. Using the unique perspective available from space, NASA will observe, monitor and assess large-scale environmental processes, focusing on climate change. MTPE satellite data, complemented by aircraft and ground data, will allow humans to better understand natural environmental changes and to distinguish natural changes from human induced changes. MTPE data, which NASA will distribute to researchers worldwide, is essential to humans making informed decisions about their environment. The goal of the Total Ozone Mapping Spectrometer (TOMS) Earth Probe mission (part of NASA's Mission To Planet Earth (MTPE) Phase I program) was to continue the high-resolution global mapping of total ozone on a daily basis (begun with the Nimbus 7 SBUV/TOMS) as well as to detect global ozone trends to verify depletion predicted by atmospheric chemistry models. The TOMS-Earth Probe (TOMS-EP), the first of a series of NASA Earth Probe missions, was one of three TOMS missions which included METEOR 3/TOMS2 (launched 1991) and ADEOS/TOMS (launched 1995). The TOMS-EP carried only one instrument: the Total Ozone Mapping Spectrometer (TOMS). The TOMS-EP spacecraft was based on the TRW/DSI Eagle bus developed under the USAF STEP program. The spacecraft was three-axis stabilized so that the TOMS instrument was nadir-pointed with about 0.5 degree control and about 0.1 degree knowledge from measured altitude data. The TOMS-EP spacecraft bus was designed to accomodate all of the TOMS instrument requirements to support a two-year lifetime with a three-year lifetime goal. The EP-TOMS Home Page is located at: http://eospso.nasa.gov/missions/total-ozone-mapping-spectrometer-earth-probe Group: Platform_Details Entry_ID: EP-TOMS Group: Platform_Identification Platform_Category: Earth Observation Satellites Short_Name: EP-TOMS Long_Name: Earth Probe-TOMS End_Group Group: Synonymous_Platform_Names Short_Name: SMEX/TOMS-Earth Probe Short_Name: Small Explorer/TOMS-Earth Probe Short_Name: TOMS-EP96 Short_Name: TOMS-Earth Probe End_Group Group: Platform_Associated_Instruments Short_Name: TOMS End_Group Group: Orbit Orbit_Altitude: 740 km Orbit_Inclination: 98.385 degrees Period: 99.6 minutes Perigee: 490.5 km Apogee: 515.2 km Orbit_Type: LEO > Low Earth Orbit > Polar Sun-Synchronous End_Group Creation_Date: 2007-05-01 Online_Resource: http://eospso.nasa.gov/missions/total-ozone-mapping-spectrometer-earth-probe Online_Resource: http://science.nasa.gov/missions/toms/ Online_Resource: http://disc.sci.gsfc.nasa.gov/acdisc/TOMS Online_Resource: https://ozoneaq.gsfc.nasa.gov/missions Group: Platform_Logistics Launch_Date: 1996-07-02 Launch_Site: Vandenberg Air Force Base, USA Design_Life: 2 years Primary_Sponsor: NASA End_Group End_Group"""@en ; skos:prefLabel "EP-TOMS"@en ; skos:inScheme ; skos:broader ; a skos:Concept .