| Names | MOS-1, Momo-1 | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Mission type | Earth observation | ||||||||||
| Operator | NASDA | ||||||||||
| COSPAR ID | 1987-018A | ||||||||||
| SATCATno. | 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 asMomo-1, wasJapan's firstEarth observation satellite. It was launched on 19 February 1987 on aN-II rocket fromTanegashima Space Center and was operated by theNational Space Development Agency of Japan (NASDA). It is in apolar orbit at roughly 900 km altitude, but was decommissioned on 29 November 1995.
It has four instruments: