VEP
Satellite information VEP
| Spacetrack Directory Name | VEP |
| Follow VEP | VEP Tracker |
| Pass predictions VEP | Pass predictions VEP |
| Orbit launches |
1994-02-03 (32 years ago)
|
| Days in orbit | 11901 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 406 km |
| Apogee | 35959 km |
| Orbit slope (inclination) | 29.2° |
| Laps per day | 2 |
| Height VEP | 24574.52 km |
Additional information VEP
VEP, 22979 is a payload satellite owned by NASDA (JP) in HEO that was launched on Thu, 03 Feb 1994 UTC via an H-II 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 VEP Date of exalting 03.02.1994y. Average height of ISS VEP hundred 24574.52 km. Average velocity VEP is 12371.01 km/h. Inclination VEP satellite 29.21°.TLE
Average velocity VEP
Average inclination VEP
Mean right ascension of the ascending node (RAAN) VEP
Mean argument of perigee VEP
Mean semi-major axis of the orbit VEP
Mean orbital eccentricity VEP
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