INTELSAT 40E
Satellite information INTELSAT 40E - 2023-052A
| Spacetrack Directory Name | INTELSAT 40E |
| Alternative name | 2023-052A |
| Follow INTELSAT 40E | INTELSAT 40E Tracker |
| Pass predictions INTELSAT 40E | Pass predictions INTELSAT 40E |
| Orbit launches |
2023-04-07 (3 years ago)
|
| Days in orbit | 1243 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 182 km |
| Apogee | 30718 km |
| Orbit slope (inclination) | 0.01° |
| Laps per day | 1 |
| Height INTELSAT 40E | 35786.38 km |
Additional information INTELSAT 40E
INTELSAT 40E, 56174 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Fri, 07 Apr 2023 UTC via an FALCON 9 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 INTELSAT 40E Date of exalting 07.04.2023y. Average height of ISS INTELSAT 40E hundred 35786.38 km. Average velocity INTELSAT 40E is 11068.94 km/h. Inclination INTELSAT 40E satellite 0.01°.TLE
Average velocity INTELSAT 40E
Average inclination INTELSAT 40E
Mean right ascension of the ascending node (RAAN) INTELSAT 40E
Mean argument of perigee INTELSAT 40E
Mean semi-major axis of the orbit INTELSAT 40E
Mean orbital eccentricity INTELSAT 40E
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