SEDSAT 1
Satellite information SEDSAT 1 - SEDSAT 1 (SO-33)
| Spacetrack Directory Name | SEDSAT 1 |
| Alternative name | SEDSAT 1 (SO-33) |
| Follow SEDSAT 1 | SEDSAT 1 Tracker |
| Pass predictions SEDSAT 1 | Pass predictions SEDSAT 1 |
| Orbit launches |
1998-10-24 (27 years ago)
|
| Days in orbit | 10180 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 542 km |
| Apogee | 1038 km |
| Orbit slope (inclination) | 31.43° |
| Laps per day | 14 |
| Height SEDSAT 1 | 785.69 km |
Additional information SEDSAT 1
SEDSAT 1, 25509 is a payload satellite owned by SEDS-HSV (US) in LEO that was launched on Sat, 24 Oct 1998 UTC via a DELTA 7326-9.5 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 SEDSAT 1 Date of exalting 24.10.1998y. Average height of ISS SEDSAT 1 hundred 785.69 km. Average velocity SEDSAT 1 is 26868.56 km/h. Inclination SEDSAT 1 satellite 31.43°.TLE
Average velocity SEDSAT 1
Average inclination SEDSAT 1
Mean right ascension of the ascending node (RAAN) SEDSAT 1
Mean argument of perigee SEDSAT 1
Mean semi-major axis of the orbit SEDSAT 1
Mean orbital eccentricity SEDSAT 1
Frequency SEDSAT 1
In the table below we show the frequencies SEDSAT 1.
| Downlink | Mode | Call sign |
|---|---|---|
| 437.910 MHz | 9k6 FSK | SEDSAT |
ISS
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