ALOUETTE 1 (S-27)
Satellite information ALOUETTE 1 (S-27) - Alouette 1
| Spacetrack Directory Name | ALOUETTE 1 (S-27) |
| Alternative name | Alouette 1 |
| Follow ALOUETTE 1 (S-27) | ALOUETTE 1 (S-27) Tracker |
| Pass predictions ALOUETTE 1 (S-27) | Pass predictions ALOUETTE 1 (S-27) |
| Orbit launches |
1962-09-29 (64 years ago)
|
| Days in orbit | 23408 |
| Country/organisation of origin | Kanada (CA) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Perigee | 986 km |
| Apogee | 1019 km |
| Orbit slope (inclination) | 80.46° |
| Laps per day | 14 |
| Height ALOUETTE 1 (S-27) | 1012.81 km |
Additional information ALOUETTE 1 (S-27)
ALOUETTE 1 (S-27), 424 is a payload satellite owned by DRTE (CA) in LEO that was launched on Sat, 29 Sep 1962 UTC via a THOR AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). 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 ALOUETTE 1 (S-27) Date of exalting 29.09.1962y. Average height of ISS ALOUETTE 1 (S-27) hundred 1012.81 km. Average velocity ALOUETTE 1 (S-27) is 26448.81 km/h. Inclination ALOUETTE 1 (S-27) satellite 80.47°.TLE
Average velocity ALOUETTE 1 (S-27)
Average inclination ALOUETTE 1 (S-27)
Mean right ascension of the ascending node (RAAN) ALOUETTE 1 (S-27)
Mean argument of perigee ALOUETTE 1 (S-27)
Mean semi-major axis of the orbit ALOUETTE 1 (S-27)
Mean orbital eccentricity ALOUETTE 1 (S-27)
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