MIDAS 7/ERS 10
Satellite information MIDAS 7/ERS 10 - Midas 9
| Spacetrack Directory Name | MIDAS 7/ERS 10 |
| Alternative name | Midas 9 |
| Follow MIDAS 7/ERS 10 | MIDAS 7/ERS 10 Tracker |
| Pass predictions MIDAS 7/ERS 10 | Pass predictions MIDAS 7/ERS 10 |
| Orbit launches |
1963-07-19 (63 years ago)
|
| Days in orbit | 23109 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Perigee | 3663 km |
| Apogee | 3739 km |
| Orbit slope (inclination) | 88.46° |
| Laps per day | 9 |
| Height MIDAS 7/ERS 10 | 3713.05 km |
Additional information MIDAS 7/ERS 10
MIDAS 7/ERS 10, 622 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Fri, 19 Jul 1963 UTC via an ATLAS AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). 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 MIDAS 7/ERS 10 Date of exalting 19.07.1963y. Average height of ISS MIDAS 7/ERS 10 hundred 3713.05 km. Average velocity MIDAS 7/ERS 10 is 22633.93 km/h. Inclination MIDAS 7/ERS 10 satellite 88.45°.TLE
Average velocity MIDAS 7/ERS 10
Average inclination MIDAS 7/ERS 10
Mean right ascension of the ascending node (RAAN) MIDAS 7/ERS 10
Mean argument of perigee MIDAS 7/ERS 10
Mean semi-major axis of the orbit MIDAS 7/ERS 10
Mean orbital eccentricity MIDAS 7/ERS 10
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