MANDRAKE 2 ABLE
Satellite information MANDRAKE 2 ABLE - 2021-059AE
| Spacetrack Directory Name | MANDRAKE 2 ABLE |
| Alternative name | 2021-059AE |
| Follow MANDRAKE 2 ABLE | MANDRAKE 2 ABLE Tracker |
| Pass predictions MANDRAKE 2 ABLE | Pass predictions MANDRAKE 2 ABLE |
| Orbit launches |
2021-06-30 g.02:00 (5 years ago)
|
| Days in orbit | 1872 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 520 km |
| Apogee | 535 km |
| Orbit slope (inclination) | 97.7° |
| Laps per day | 16 |
| Height MANDRAKE 2 ABLE | 430.66 km |
Additional information MANDRAKE 2 ABLE
MANDRAKE 2 ABLE, 48907 is an American payload satellite in SSO that was launched on Wed, 30 Jun 2021 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 MANDRAKE 2 ABLE Date of exalting 30.06.2021y. Average height of ISS MANDRAKE 2 ABLE hundred 430.66 km. Average velocity MANDRAKE 2 ABLE is 27556.6 km/h. Inclination MANDRAKE 2 ABLE satellite 97.7°.TLE
Average velocity MANDRAKE 2 ABLE
Average inclination MANDRAKE 2 ABLE
Mean right ascension of the ascending node (RAAN) MANDRAKE 2 ABLE
Mean argument of perigee MANDRAKE 2 ABLE
Mean semi-major axis of the orbit MANDRAKE 2 ABLE
Mean orbital eccentricity MANDRAKE 2 ABLE
Frequency MANDRAKE 2 ABLE
In the table below we show the frequencies MANDRAKE 2 ABLE.
| Downlink | Mode |
|---|---|
| 400.498 MHz | FSK |
ISS
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