TELKOMSAT 113BT
Satellite information TELKOMSAT 113BT - 2024-035A
| Spacetrack Directory Name | TELKOMSAT 113BT |
| Alternative name | 2024-035A |
| Follow TELKOMSAT 113BT | TELKOMSAT 113BT Tracker |
| Pass predictions TELKOMSAT 113BT | Pass predictions TELKOMSAT 113BT |
| Orbit launches |
2024-02-20 (2 years ago)
|
| Days in orbit | 921 |
| Country/organisation of origin | Indonezja (INDO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 317 km |
| Apogee | 54924 km |
| Orbit slope (inclination) | 0.02° |
| Laps per day | 1 |
| Height TELKOMSAT 113BT | 35786.5 km |
Additional information TELKOMSAT 113BT
TELKOMSAT 113BT, 58995 is a payload satellite owned by Telkom (ID) in GEO that was launched on Tue, 20 Feb 2024 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 TELKOMSAT 113BT Date of exalting 20.02.2024y. Average height of ISS TELKOMSAT 113BT hundred 35786.5 km. Average velocity TELKOMSAT 113BT is 11068.92 km/h. Inclination TELKOMSAT 113BT satellite 0.02°.TLE
Average velocity TELKOMSAT 113BT
Average inclination TELKOMSAT 113BT
Mean right ascension of the ascending node (RAAN) TELKOMSAT 113BT
Mean argument of perigee TELKOMSAT 113BT
Mean semi-major axis of the orbit TELKOMSAT 113BT
Mean orbital eccentricity TELKOMSAT 113BT
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