SES 1
Satellite information SES 1 - SES-1
| Spacetrack Directory Name | SES 1 |
| Alternative name | SES-1 |
| Group | SES |
| Follow SES 1 | SES 1 Tracker |
| Group follow SES | Tracker SES |
| Pass predictions SES 1 | Pass predictions SES 1 |
| Orbit launches |
2010-04-24 (16 years ago)
|
| Days in orbit | 5949 |
| Country/organisation of origin | SES |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Type | Satellite |
| Categories | |
| Perigee | 35776 km |
| Apogee | 35797 km |
| Orbit slope (inclination) | 0.06° |
| Laps per day | 1 |
| Orbit | GEO |
| Height SES 1 | 35786.14 km |
Additional information SES 1
SES-1 is a communication satellite owned by SESSL, manufactured by OSCD and based on the OSC Star 2.4 bus configuration. Launched from TYMSC at LC200/39 using a Proton-M/Briz-M launch vehicle on April 24, 2010, SES-1 has a dry mass of 1,180 kg and was launched with a total mass of 2,561 kg. The satellite is equipped with 2 deployable solar arrays and batteries for power supply, featuring 24 active C-band transponders, 24 Ku-band transponders, and Ka-band transponders. It also includes CHIRP technology (specific to SES-1 #2). SES-1 measures 3.2 meters in length, has a diameter of 2.3 meters, and spans 22 meters with its solar arrays deployed. The satellites shape is described as Box + 2 Pan, with a radar cross-section (RCS) of 26.9753. It was designed for a mission lifetime of 15 years, fueled for over 16 years.
satellite SES 1 Date of exalting 24.04.2010y. Average height of ISS SES 1 hundred 35786.14 km. Average velocity SES 1 is 11068.98 km/h. Inclination SES 1 satellite 0.03°.TLE
Average orbit height SES 1
Average velocity SES 1
Average inclination SES 1
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