INTELSAT 35E
Satellite information INTELSAT 35E - INTELSAT 35E (IS-35E)
| Spacetrack Directory Name | INTELSAT 35E |
| Alternative name | INTELSAT 35E (IS-35E) |
| Group | INTELSAT |
| Follow INTELSAT 35E | INTELSAT 35E Tracker |
| Group follow INTELSAT | Tracker INTELSAT |
| Pass predictions INTELSAT 35E | Pass predictions INTELSAT 35E |
| Orbit launches |
2017-07-05 (9 years ago)
|
| Days in orbit | 3411 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 35778 km |
| Apogee | 35795 km |
| Orbit slope (inclination) | 0° |
| Laps per day | 1 |
| Orbit | GEO |
| Height INTELSAT 35E | 35786.44 km |
Additional information INTELSAT 35E
INTELSAT 35E (IS-35E) is a communication satellite owned by INTELU and was launched on July 5, 2017, from LC39A at AFETR using a Falcon 9 launch vehicle. It has dimensions of 7.5 meters in length, 3 meters in diameter, and spans 44 meters with its solar arrays deployed. The satellites dry mass is 3500 kg, and it was launched with a total mass of 6761 kg. Equipped with C-band and Ku-band high-throughput transponders for communication purposes, IS-35E is powered by two deployable solar arrays and batteries. It operates on a BSS-702MP bus manufactured by BOES and features an IHI BT-4 motor. The satellites shape includes a box with two panels and its intended lifetime is 15 years.
satellite INTELSAT 35E Date of exalting 05.07.2017y. Average height of ISS INTELSAT 35E hundred 35786.44 km. Average velocity INTELSAT 35E is 11068.93 km/h. Inclination INTELSAT 35E satellite 0.02°.TLE
Average velocity INTELSAT 35E
Average inclination INTELSAT 35E
Mean right ascension of the ascending node (RAAN) INTELSAT 35E
Mean argument of perigee INTELSAT 35E
Mean semi-major axis of the orbit INTELSAT 35E
Mean orbital eccentricity INTELSAT 35E
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