SYNCOM 2 (A 26)
Satellite information SYNCOM 2 (A 26) - A 26
| Spacetrack Directory Name | SYNCOM 2 (A 26) |
| Alternative name | A 26 |
| Follow SYNCOM 2 (A 26) | SYNCOM 2 (A 26) Tracker |
| Pass predictions SYNCOM 2 (A 26) | Pass predictions SYNCOM 2 (A 26) |
| Orbit launches |
1963-07-26 (63 years ago)
|
| Days in orbit | 23058 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 35761 km |
| Apogee | 35807 km |
| Orbit slope (inclination) | 29.8° |
| Laps per day | 1 |
| Height SYNCOM 2 (A 26) | 35788.58 km |
Additional information SYNCOM 2 (A 26)
SYNCOM 2 (A 26), 634 is a payload satellite owned by GSFC (US) in GEO that was launched on Fri, 26 Jul 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 SYNCOM 2 (A 26) Date of exalting 26.07.1963y. Average height of ISS SYNCOM 2 (A 26) hundred 35788.58 km. Average velocity SYNCOM 2 (A 26) is 11068.92 km/h. Inclination SYNCOM 2 (A 26) satellite 29.84°.TLE
Average velocity SYNCOM 2 (A 26)
Average inclination SYNCOM 2 (A 26)
Mean right ascension of the ascending node (RAAN) SYNCOM 2 (A 26)
Mean argument of perigee SYNCOM 2 (A 26)
Mean semi-major axis of the orbit SYNCOM 2 (A 26)
Mean orbital eccentricity SYNCOM 2 (A 26)
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