INTELSAT 29E
Satellite information INTELSAT 29E - INTELSAT 29E (IS-29E)
| Spacetrack Directory Name | INTELSAT 29E |
| Alternative name | INTELSAT 29E (IS-29E) |
| Follow INTELSAT 29E | INTELSAT 29E Tracker |
| Pass predictions INTELSAT 29E | Pass predictions INTELSAT 29E |
| Orbit launches |
2016-01-27 (10 years ago)
|
| Days in orbit | 3863 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| WWW | Here |
| Perigee | 35644 km |
| Apogee | 35737 km |
| Orbit slope (inclination) | 6.66° |
| Laps per day | 1 |
| Orbit | GEO |
| Height INTELSAT 29E | 35685.16 km |
Additional information INTELSAT 29E
INTELSAT 29E, 41308 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Wed, 27 Jan 2016 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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 INTELSAT 29E Date of exalting 27.01.2016y. Average height of ISS INTELSAT 29E hundred 35685.16 km. Average velocity INTELSAT 29E is 11082.26 km/h. Inclination INTELSAT 29E satellite 6.65°.TLE
Average velocity INTELSAT 29E
Average inclination INTELSAT 29E
Mean right ascension of the ascending node (RAAN) INTELSAT 29E
Mean argument of perigee INTELSAT 29E
Mean semi-major axis of the orbit INTELSAT 29E
Mean orbital eccentricity INTELSAT 29E
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