| 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.
It has four instruments: