TURKMENALEM52E/MONACOSAT - Norad ID: 40617
| Spacetrack Directory Name | TURKMENALEM 52E/MONACOSA |
| Alternative name | TURKMENALEM52E/MONACOSAT |
| Follow TURKMENALEM 52E/MONACOSA | TURKMENALEM 52E/MONACOSA Tracker |
| Pass predictions TURKMENALEM 52E/MONACOSA | Pass predictions TURKMENALEM 52E/MONACOSA |
| Orbit launches |
|
| Days in orbit | 4029 |
| Country/organisation of origin | Turkmenistan, Monako (TMMC) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Categories | |
| Perigee | 35773 km |
| Apogee | 35799 km |
| Orbit slope (inclination) | 0.04° |
| Laps per day | 1 |
| Orbit | GEO |
| Height TURKMENALEM 52E/MONACOSA | 35785.97 km |
TURKMENALEM 52E/MONACOSA, 40617 is a TM and MC payload satellite in GEO that was launched on Mon, 27 Apr 2015 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 TURKMENALEM 52E/MONACOSA Date of exalting 27.04.2015y. Average height of ISS TURKMENALEM 52E/MONACOSA hundred 35785.97 km. Average velocity TURKMENALEM 52E/MONACOSA is 11068.99 km/h. Inclination TURKMENALEM 52E/MONACOSA satellite 0.03°.