ELEKTRON 3
Satellite information ELEKTRON 3
| Spacetrack Directory Name | ELEKTRON 3 |
| Follow ELEKTRON 3 | ELEKTRON 3 Tracker |
| Pass predictions ELEKTRON 3 | Pass predictions ELEKTRON 3 |
| Orbit launches |
1964-07-10 (62 years ago)
|
| Days in orbit | 22757 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 412 km |
| Apogee | 6156 km |
| Orbit slope (inclination) | 60.81° |
| Laps per day | 9 |
| Height ELEKTRON 3 | 3654.86 km |
Additional information ELEKTRON 3
ELEKTRON 3, 829 is a payload satellite owned by OKB-1 (CIS) that was launched on Fri, 10 Jul 1964 UTC via a VOSTOK 8K72 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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 ELEKTRON 3 Date of exalting 10.07.1964y. Average height of ISS ELEKTRON 3 hundred 3654.86 km. Average velocity ELEKTRON 3 is 22675.8 km/h. Inclination ELEKTRON 3 satellite 60.81°.TLE
Average velocity ELEKTRON 3
Average inclination ELEKTRON 3
Mean right ascension of the ascending node (RAAN) ELEKTRON 3
Mean argument of perigee ELEKTRON 3
Mean semi-major axis of the orbit ELEKTRON 3
Mean orbital eccentricity ELEKTRON 3
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