SHINSEI (MS-F2)
Satellite information SHINSEI (MS-F2)
| Spacetrack Directory Name | SHINSEI (MS-F2) |
| Follow SHINSEI (MS-F2) | SHINSEI (MS-F2) Tracker |
| Pass predictions SHINSEI (MS-F2) | Pass predictions SHINSEI (MS-F2) |
| Orbit launches |
1971-09-28 g.01:00 (55 years ago)
|
| Days in orbit | 20097 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | KSCUT (Uchinoura Space Center, Japan) |
| WWW | Here |
| Perigee | 870 km |
| Apogee | 1861 km |
| Orbit slope (inclination) | 32.06° |
| Laps per day | 13 |
| Height SHINSEI (MS-F2) | 1381.99 km |
Additional information SHINSEI (MS-F2)
SHINSEI (MS-F2), 5485 is a payload satellite owned by ISAS (JP) in LEO that was launched on Tue, 28 Sep 1971 UTC via a MU-4S launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). 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 SHINSEI (MS-F2) Date of exalting 28.09.1971y. Average height of ISS SHINSEI (MS-F2) hundred 1381.99 km. Average velocity SHINSEI (MS-F2) is 25814.04 km/h. Inclination SHINSEI (MS-F2) satellite 32.05°.TLE
Average velocity SHINSEI (MS-F2)
Average inclination SHINSEI (MS-F2)
Mean right ascension of the ascending node (RAAN) SHINSEI (MS-F2)
Mean argument of perigee SHINSEI (MS-F2)
Mean semi-major axis of the orbit SHINSEI (MS-F2)
Mean orbital eccentricity SHINSEI (MS-F2)
Frequency SHINSEI (MS-F2)
In the table below we show the frequencies SHINSEI (MS-F2).
| Downlink | Mode |
|---|---|
| 136.694 MHz | CW |
ISS
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