Suggested Edit for Satellite
Suggested by ea7koo on: 2022-04-30 18:15
Citation: https://www.researchgate.net/publication/325152032_NANOSATELLITE_EAGLET-1_READY_FOR_LAUNCH
Verdict: Approved
Reviewed by - on: 2022-05-01 12:08
| Name | Eaglet 1 |
| NORAD ID | 43790 |
| Followed NORAD ID | - |
| Alternative Names | - |
| Description | Eaglet 1 is the first nanosatellite by OHB Italia SpA for Earth Observation. Eaglet 1 is a 3U+ cubesat with 5 m panchromatic resolution capabilities, using a 300 mm focal length telescope with an aperture of 85 mm. The overall mass is less than 5 kg. The satellite has a precise attitude control system based on Earth, Sun, Star Tracker and GPS sensors. The attitude control system makes use of reaction wheel and utilizes magneto-torquers for their desaturation. In addition to the EO mission, Eaglet shall embark an AIS-receiver. |
| Owner/Operator | - |
| Status |
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| Countries of Origin | |
| Website | - |
| Dashboard URL | - |
| Launch Date | Dec. 3, 2018, midnight |
| Deploy Date | - |
| Image |  |
| Field | Previous | Suggested |
|---|---|---|
| Name | Eaglet-I | Eaglet 1 |
| Description | - | Eaglet 1 is the first nanosatellite by OHB Italia SpA for Earth Observation. Eaglet 1 is a 3U+ cubesat with 5 m panchromatic resolution capabilities, using a 300 mm focal length telescope with an aperture of 85 mm. The overall mass is less than 5 kg. The satellite has a precise attitude control system based on Earth, Sun, Star Tracker and GPS sensors. The attitude control system makes use of reaction wheel and utilizes magneto-torquers for their desaturation. In addition to the EO mission, Eaglet shall embark an AIS-receiver. |
| Launch Date | - | Dec. 3, 2018, midnight |
| Image |
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