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 |
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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:
- "Multi-Spectral Electronic Self-Scanning Radiometer (MESSR)" which offers 50 m resolution in two visible and two infra-red spectral bands over two 100 km swathes.
- "Visible and Thermal Infrared Radiometer (VTIR)" which has a much lower resolution in one visible and three infrared bands over a 1,500 km swathe.
- "Micro Scanning Radiometer (MSR)" which measures microwave emission in the 23 GHz and 31 GHz bands.
- "Data Collection System (DCS)" which is an experimental transponder.[7]
External links
Notes and References
- Book: Ninomiya, Keiken . Automatic Control in Aerospace 2004 . . Proceedings of the 16th IFAC Symposium, Volume 1 . Alexander . Nebylov . 199 . 2005 . 0-08-044013-4.
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
- Web site: JAXA | N-II Launch Vehicle.
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayExperiment.action?spacecraftId=1987-018A - 24 January 2020