TELSTAR 2 (A-41)
Satellite information TELSTAR 2 (A-41) - A-41
| Spacetrack Directory Name | TELSTAR 2 (A-41) |
| Alternative name | A-41 |
| Follow TELSTAR 2 (A-41) | TELSTAR 2 (A-41) Tracker |
| Pass predictions TELSTAR 2 (A-41) | Pass predictions TELSTAR 2 (A-41) |
| Orbit launches |
1963-05-07 (63 years ago)
|
| Days in orbit | 23138 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 968 km |
| Apogee | 10803 km |
| Orbit slope (inclination) | 42.76° |
| Laps per day | 6 |
| Height TELSTAR 2 (A-41) | 6871.77 km |
Additional information TELSTAR 2 (A-41)
TELSTAR 2 (A-41), 573 is a payload satellite owned by AT&T (US) in HEO that was launched on Tue, 07 May 1963 UTC via a THOR DELTA B launch vehicle from the Air Force Eastern Test Range (AFETR). 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 TELSTAR 2 (A-41) Date of exalting 07.05.1963y. Average height of ISS TELSTAR 2 (A-41) hundred 6871.77 km. Average velocity TELSTAR 2 (A-41) is 19682.16 km/h. Inclination TELSTAR 2 (A-41) satellite 42.76°.TLE
Average velocity TELSTAR 2 (A-41)
Average inclination TELSTAR 2 (A-41)
Mean right ascension of the ascending node (RAAN) TELSTAR 2 (A-41)
Mean argument of perigee TELSTAR 2 (A-41)
Mean semi-major axis of the orbit TELSTAR 2 (A-41)
Mean orbital eccentricity TELSTAR 2 (A-41)
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