A | B | C | D | E | F | G | H | CH | I | J | K | L | M | N | O | P | Q | R | S | T | U | V | W | X | Y | Z | 0 | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9
Names | MOS-1, Momo-1 | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|
Mission type | Earth observation | ||||||||||
Operator | NASDA | ||||||||||
COSPAR ID | 1987-018A | ||||||||||
SATCAT no. | 17527 | ||||||||||
Mission duration | Planned: 2 years Final: 8 years, 9 months, 9 days | ||||||||||
Spacecraft properties | |||||||||||
Manufacturer | NEC[1] | ||||||||||
Launch mass | 750 kg [2] | ||||||||||
Start of mission | |||||||||||
Launch date | 19 February 1987 01:23:00 UTC [3] | ||||||||||
Rocket | N-II (N-16F) [4] | ||||||||||
Launch site | Tanegashima LC-N | ||||||||||
Contractor | NASDA | ||||||||||
End of mission | |||||||||||
Disposal | Decommissioned | ||||||||||
Deactivated | 29 November 1995 | ||||||||||
Orbital parameters | |||||||||||
Reference system | Geocentric | ||||||||||
Regime | Sun-synchronous | ||||||||||
Perigee altitude | 909 km [5] | ||||||||||
Apogee altitude | 909 km | ||||||||||
Inclination | 99.1° | ||||||||||
Period | 103.2 minutes | ||||||||||
| |||||||||||
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]
References
- ^ Ninomiya, Keiken (2005). Nebylov, Alexander (ed.). Automatic Control in Aerospace 2004. Proceedings of the 16th IFAC Symposium, Volume 1. Elsevier. p. 199. ISBN 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
- ^ "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
External links
- MOS-1 site by JAXA
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