AMC-3 (GE-3)
Satellite information AMC-3 (GE-3) - GE-3r
| Spacetrack Directory Name | AMC-3 (GE-3) |
| Alternative name | GE-3r |
| Group | SES |
| Follow AMC-3 (GE-3) | AMC-3 (GE-3) Tracker |
| Group follow SES | Tracker SES |
| Pass predictions AMC-3 (GE-3) | Pass predictions AMC-3 (GE-3) |
| Orbit launches |
1997-09-04 (28 years ago)
|
| Days in orbit | 10517 |
| Country/organisation of origin | SES |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Type | Satellite |
| Categories | |
| Perigee | 35773 km |
| Apogee | 35801 km |
| Orbit slope (inclination) | 8.17° |
| Laps per day | 1 |
| Orbit | GEO |
| Height AMC-3 (GE-3) | 35794.08 km |
Additional information AMC-3 (GE-3)
AMC-3 (also known as GE 3) is a communication satellite with a NORAD catalog ID of 24936 and an object ID of 1997-050A, operated by AMCG. It was launched on September 4, 1997, from the Air Force Eastern Test Range (AFETR), using the Atlas IIAS launch vehicle from Launch Complex 36A. The satellite has a box shape with two panels and is equipped with 2 deployable solar arrays and batteries for power generation. It carries 24 C-band transponders and 24 Ku-band transponders, weighing 1300 kg dry and 2845 kg at launch. Manufactured by LMTEW (Lockheed Martin Telecommunications & Electronics West), AMC-3 was designed to operate for a 15-year lifetime with a Leros 1C motor. Its dimensions are 2.6 meters in length, 1.8 meters in diameter, and spans 22 meters when deployed.
satellite AMC-3 (GE-3) Date of exalting 04.09.1997y. Average height of ISS AMC-3 (GE-3) hundred 35794.08 km. Average velocity AMC-3 (GE-3) is 11067.96 km/h. Inclination AMC-3 (GE-3) satellite 7.7°.TLE
Average orbit height AMC-3 (GE-3)
Average velocity AMC-3 (GE-3)
Average inclination AMC-3 (GE-3)
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