MOS-1 (satellite) explained

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Marine Observation Satellite-1
Names List:MOS-1, Momo-1
Mission Type:Earth observation
Operator:NASDA
Cospar Id:1987-018A
Satcat:17527
Mission Duration:Planned: 2 years
Final:
Manufacturer:NEC[1]
Launch Mass:750 kg [2]
Launch Date:19 February 1987
01:23:00 UTC [3]
Launch Rocket:N-II (N-16F) [4]
Launch Site:Tanegashima LC-N
Launch Contractor:NASDA
Disposal Type:Decommissioned
Deactivated:29 November 1995
Orbit Reference:Geocentric
Orbit Regime:Sun-synchronous
Orbit Periapsis:909 km [5]
Orbit Apoapsis:909 km
Orbit Inclination:99.1°
Orbit Period:103.2 minutes
Apsis:gee
Instruments List:
Acronym1:MESSR
Name1:Multispectral Electronic Self-Scanning Radiometer [6]
Acronym2:VTIR
Name2:Visible and Thermal Infrared Radiometer
Acronym3:MSR
Name3:Microwave Scanning Radiometer
Acronym4:DCS
Name4:Data Collection System

Marine Observation Satellite-1 (MOS-1), also known as Momo-1, was Japan's first Earth observation satellite. It was launched on 19 February 1987 on a N-II rocket from Tanegashima Space Center and was operated by the National Space Development Agency of Japan (NASDA). It is in a polar orbit at roughly 900 km altitude, but was decommissioned on 29 November 1995.

Instruments

It has four instruments:

External links

Notes and References

  1. Book: Ninomiya, Keiken . Automatic Control in Aerospace 2004 . . Proceedings of the 16th IFAC Symposium, Volume 1 . Alexander . Nebylov . 199 . 2005 . 0-08-044013-4.
  2. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1987-018A - 24 January 2020
  3. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
  4. Web site: JAXA | N-II Launch Vehicle.
  5. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
  6. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020
  7. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020