UME 2 (ISS-B)
Satellite information UME 2 (ISS-B)
| Spacetrack Directory Name | UME 2 (ISS-B) |
| Follow UME 2 (ISS-B) | UME 2 (ISS-B) Tracker |
| Pass predictions UME 2 (ISS-B) | Pass predictions UME 2 (ISS-B) |
| Orbit launches |
1978-02-16 (48 years ago)
|
| Days in orbit | 17732 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 976 km |
| Apogee | 1216 km |
| Orbit slope (inclination) | 69.36° |
| Laps per day | 13 |
| Height UME 2 (ISS-B) | 1106.78 km |
Additional information UME 2 (ISS-B)
UME 2 (ISS-B), 10674 is a payload satellite owned by NASDA (JP) in LEO that was launched on Thu, 16 Feb 1978 UTC via an N-1 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 UME 2 (ISS-B) Date of exalting 16.02.1978y. Average height of ISS UME 2 (ISS-B) hundred 1106.78 km. Average velocity UME 2 (ISS-B) is 26282.74 km/h. Inclination UME 2 (ISS-B) satellite 69.36°.TLE
Average velocity UME 2 (ISS-B)
Average inclination UME 2 (ISS-B)
Mean right ascension of the ascending node (RAAN) UME 2 (ISS-B)
Mean argument of perigee UME 2 (ISS-B)
Mean semi-major axis of the orbit UME 2 (ISS-B)
Mean orbital eccentricity UME 2 (ISS-B)
ISS
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