MOS 1A (MOMO 1)
Satellite information MOS 1A (MOMO 1) - MOMO-1 (MOS-1)
| Spacetrack Directory Name | MOS 1A (MOMO 1) |
| Alternative name | MOMO-1 (MOS-1) |
| Follow MOS 1A (MOMO 1) | MOS 1A (MOMO 1) Tracker |
| Pass predictions MOS 1A (MOMO 1) | Pass predictions MOS 1A (MOMO 1) |
| Orbit launches |
1987-02-19 (39 years ago)
|
| Days in orbit | 14442 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 879 km |
| Apogee | 891 km |
| Orbit slope (inclination) | 98.83° |
| Laps per day | 14 |
| Height MOS 1A (MOMO 1) | 894.54 km |
Additional information MOS 1A (MOMO 1)
MOS 1A (MOMO 1), 17527 is a payload satellite owned by NASDA (JP) in SSO that was launched on Thu, 19 Feb 1987 UTC via an N-2 launch vehicle from the Tanegashima Space Center (TNSTA). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite MOS 1A (MOMO 1) Date of exalting 19.02.1987y. Average height of ISS MOS 1A (MOMO 1) hundred 894.54 km. Average velocity MOS 1A (MOMO 1) is 26663.05 km/h. Inclination MOS 1A (MOMO 1) satellite 98.84°.TLE
Average velocity MOS 1A (MOMO 1)
Average inclination MOS 1A (MOMO 1)
Mean right ascension of the ascending node (RAAN) MOS 1A (MOMO 1)
Mean argument of perigee MOS 1A (MOMO 1)
Mean semi-major axis of the orbit MOS 1A (MOMO 1)
Mean orbital eccentricity MOS 1A (MOMO 1)
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