@prefix skos: <http://www.w3.org/2004/02/skos/core#> .
@prefix ns0: <http://gcmd.gsfc.nasa.gov/kms#> .

<https://gcmd.earthdata.nasa.gov/kms/concept/949ab40f-3954-4c81-a063-275d0e13a14e>
  skos:prefLabel "INSAT (Indian National Satellite)"@en ;
  a skos:Concept ;
  skos:narrower <https://gcmd.earthdata.nasa.gov/kms/concept/9dfe63d1-5b6a-4ac4-ae19-1572ab43445e> .

<https://gcmd.earthdata.nasa.gov/kms/concept/9dfe63d1-5b6a-4ac4-ae19-1572ab43445e>
  ns0:altLabel [ ] ;
  skos:definition """Spacecraft Brief Description
    The  Insat 1B was the second spacecraft in the first generation Indian
    National  Satellite  System.   The  three-axis  stabilized spacecraft,
    originally  launched  as  an on-orbit backup, replaced Insat 1A, which
    failed  in  late 1982.  It was positioned in a geosynchronous orbit at
    74  deg  E with a host of ground stations throughout India.  The Insat
    1B   satellite,   built  by  the  Ford  Aerospace  and  Communications
    Corporation,  was  designed  to  provide  combined telecommunications,
    direct  TV  broadcast,  and meteorological service to India's civilian
    community  over  a  7-year-in-orbit  lifespan.  The telecommunications
    package  provided two-way, long-distance telephone circuits and direct
    radio  and  TV  broadcasting  to  the  remotest  areas  of India.  The
    meteorology  package was comprised of a scanning very-high-resolution,
    two-channel   radiometer  (VHRR)  to  provide  full-frame,  full-earth
    coverage  every 30 min.  The visual channel (0.55-0.75 micrometer) had
    a  2.75-km resolution while the IR channel (10.5-12.5 micrometers) had
    an 11-km resolution.  Using the Insat TV capability, early warnings of
    impending  disasters  (i.e.,  floods, storms, etc.) can directly reach
    the  civilian population, even in remote areas.  The Insat 1B also had
    a   data   channel  for  relaying  meteorological,  hydrological,  and
    oceanographic  data  from  unattended  land-based  or ocean-based data
    collection and transmission platforms.
* INSAT-1B was relegated to spare status on 17 July 1990 by the
  INSAT-1D. The INSAT-1B was finally removed from GEO in August 1993,
  after being replaced at 93.50E by INSAT-2B.*
  Auxiliary Information
    Launch Date and Time : 1983-08-31 07:49:00
    Epoch Date and Time :  1983-10-15
    Orbit Type :  Geocentric
    Apogee(km) :   35680.
    Perigee(km) :  35680.
    Inclination :     0.0
    Date of last update :  1998-10-07
More information about the INSAT Satellite Series is available at:
"http://www.bharat-rakshak.com/SPACE/space-satellite3.html"


Group: Platform_Details
   Entry_ID: INSAT-1B
   Group: Platform_Identification
      Platform_Category: Earth Observation Satellites
      Platform_Series_or_Entity: INSAT (Indian National Satellite)
      Short_Name: INSAT-1B
      Long_Name: Indian National Satellite-1B
   End_Group
   Group: Synonymous_Platform_Names
      Short_Name: INSAT-1B
   End_Group
   Group: Platform_Associated_Instruments
      Short_Name: VHRR
   End_Group
   Group: Orbit
      Orbit_Inclination: 0.0
      Perigee: 35680
      Apogee: 35680
   End_Group
   Creation_Date: 2007-10-05
   Online_Resource: http://www.bharat-rakshak.com/SPACE/space-satellite3.html
   Group: Platform_Logistics
      Launch_Date: 1983-08-31
      Primary_Sponsor: India
   End_Group
End_Group"""@en ;
  skos:prefLabel "INSAT-1B"@en ;
  skos:inScheme <https://gcmd.earthdata.nasa.gov/kms/concepts/concept_scheme/platforms> ;
  skos:broader <https://gcmd.earthdata.nasa.gov/kms/concept/949ab40f-3954-4c81-a063-275d0e13a14e> ;
  a skos:Concept .

